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Cooperative Path Planning of Unmanned Aerial Vehicles
by Antonios Tsourdos
Part 32 of the Aerospace series
An invaluable addition to the literature on UAV guidance and cooperative control, Cooperative Path Planning of Unmanned Aerial Vehicles is a dedicated, practical guide to computational path planning for UAVs. One of the key issues facing future development of UAVs is path planning: it is vital that swarm UAVs/ MAVs can cooperate together in a coordinated manner, obeying a pre-planned course but able to react to their environment by communicating and cooperating. An optimized path is necessary in order to ensure a UAV completes its mission efficiently, safely, and successfully.
Focussing on the path planning of multiple UAVs for simultaneous arrival on target, Cooperative Path Planning of Unmanned Aerial Vehicles also offers coverage of path planners that are applicable to land, sea, or space-borne vehicles.
Cooperative Path Planning of Unmanned Aerial Vehicles is authored by leading researchers from Cranfield University and provides an authoritative resource for researchers, academics and engineers working in the area of cooperative systems, cooperative control and optimization particularly in the aerospace industry.
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Advanced Control of Aircraft, Spacecraft and Rockets
by Ashish Tewari
Part 37 of the Aerospace series
“Advanced Control of Aircraft, Spacecraft and Rockets” introduces the reader to the concepts of modern control theory applied to the design and analysis of general flight control systems in a concise and mathematically rigorous style. It presents a comprehensive treatment of both atmospheric and space flight control systems including aircraft, rockets (missiles and launch vehicles), entry vehicles and spacecraft (both orbital and attitude control). The broad coverage of topics emphasizes the synergies among the various flight control systems and attempts to show their evolution from the same set of physical principles as well as their design and analysis by similar mathematical tools. In addition, this book presents state-of-art control system design methods-including multivariable, optimal, robust, digital and nonlinear strategies-as applied to modern flight control systems.
“Advanced Control of Aircraft, Spacecraft and Rockets” features worked examples and problems at the end of each chapter as well as a number of MATLAB / Simulink examples that are realistic and representative of the state-of-the-art in flight control.
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Basic Helicopter Aerodynamics
by John M. Seddon
Part 40 of the Aerospace series
“Basic Helicopter Aerodynamics” is widely appreciated as an easily accessible, rounded introduction to the first principles of the aerodynamics of helicopter flight. Simon Newman has brought this third edition completely up to date with a full new set of illustrations and imagery.
Simon Newman addresses the unique considerations applicable to rotor UAVs and MAVs, and coverage of blade dynamics is expanded to include both flapping, lagging and ground resonance. New material is included on blade tip design, flow characteristics surrounding the rotor in forward flight, tail rotors, brown-out, blade sailing and shipborne operations.
Concentrating on the well-known Sikorsky configuration of single main rotor with tail rotor, early chapters deal with the aerodynamics of the rotor in hover, vertical flight, forward flight and climb. Analysis of these motions is developed to the stage of obtaining the principal results for thrust, power and associated quantities. Later chapters turn to the characteristics of the overall helicopter, its performance, stability and control, and the important field of aerodynamic research is discussed, with some reference also to aerodynamic design practice.
This introductory level treatment to the aerodynamics of helicopter flight will appeal to aircraft design engineers and undergraduate and graduate students in aircraft design, as well as practicing engineers looking for an introduction to or refresher course on the subject.
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Principles of Flight for Pilots
by Peter J. Swatton
Part 42 of the Aerospace series
Organised and written as an accessible study guide for student pilots wishing to take commercial ground examinations to obtain ATPL or CPL licenses, “Principles of Flight for Pilots” also provides a reliable up-to-date reference for qualified and experienced personnel wishing to further improve their understanding of the Principles of Flight and related subjects. Providing a unique aerodynamics reference tool, unlike any book previously Principles of Flight for Pilots explains in significant depth all the topics necessary to pass the Principles of Flight examination as required by the EASA syllabus.
Aviation ground instructor Peter J. Swatton, well reputed for his previous works in the field of pilot ground training, presents the subject in seven parts including basic aerodynamics; level flight aerodynamics; stability; manoeuvre aerodynamics; and other aerodynamic considerations. Each chapter includes self-assessed questions, 848 in total spread over eighteen chapters, with solutions provided at the end of the book containing full calculations and explanations.
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Air Travel and Health
A Systems Perspective
by Allan Seabridge
Part 44 of the Aerospace series
Providing a detailed examination of the issues that affect the long-term health of aircrew, cabin crew and passengers, Air Travel and Health offers guidance to engineers designing aircraft in the difficult field of legislation and product liability. Examining the facts, anecdotes and myths associated with health and travel, Seabridge and Morgan draw balanced conclusions on which the aircraft operations and design communities can act to provide cost-effective solutions. The authors present a useful reference for aircrew, regulatory authorities, engineers and managers within the aerospace industry, and medical and human factor specialists, as well as an informative resource for undergraduate and graduate students.
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Gas Turbine Propulsion Systems
by Bernie Macisaac
Part 49 of the Aerospace series
Major changes in gas turbine design, especially in the design and complexity of engine control systems, have led to the need for an up to date, systems-oriented treatment of gas turbine propulsion. Pulling together all of the systems and subsystems associated with gas turbine engines in aircraft and marine applications, Gas Turbine Propulsion Systems discusses the latest developments in the field.
Chapters include aircraft engine systems functional overview, marine propulsion systems, fuel control and power management systems, engine lubrication and scavenging systems, nacelle and ancillary systems, engine certification, unique engine systems and future developments in gas turbine propulsion systems. The authors also present examples of specific engines and applications.
Written from a wholly practical perspective by two authors with long careers in the gas turbine & fuel systems industries, Gas Turbine Propulsion Systems provides an excellent resource for project and program managers in the gas turbine engine community, the aircraft OEM community, and tier 1 equipment suppliers in Europe and the United States. It also offers a useful reference for students and researchers in aerospace engineering.
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Aircraft Systems
Mechanical, Electrical, and Avionics Subsystems Integration
by Ian Moir
Part 52 of the Aerospace series
This third edition of Aircraft Systems represents a timely update of the Aerospace Series' successful and widely acclaimed flagship title. Moir and Seabridge present an in-depth study of the general systems of an aircraft — electronics, hydraulics, pneumatics, emergency systems and flight control to name but a few - that transform an aircraft shell into a living, functioning and communicating flying machine. Advances in systems technology continue to alloy systems and avionics, with aircraft support and flight systems increasingly controlled and monitored by electronics, the authors handle the complexities of these overlaps and interactions in a straightforward and accessible manner that also enhances synergy with the book's two sister volumes, Civil Avionics Systems and Military Avionics Systems.
Aircraft Systems, 3rd Edition is thoroughly revised and expanded from the last edition in 2001, reflecting the significant technological and procedural changes that have occurred in the interim — new aircraft types, increased electronic implementation, developing markets, increased environmental pressures and the emergence of UAVs. Every chapter is updated, and the latest technologies depicted. It offers an essential reference tool for aerospace industry researchers and practitioners such as aircraft designers, fuel specialists, engine specialists, and ground crew maintenance providers, as well as a textbook for senior undergraduate and postgraduate students in systems engineering, aerospace and engineering avionics.
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Unmanned Aircraft Systems
UAVS Design, Development and Deployment
by Reg Austin
Part 54 of the Aerospace series
Unmanned Aircraft Systems delivers a much needed introduction to UAV System technology, taking an integrated approach that avoids compartmentalising the subject. Arranged in four sections, parts 1-3 examine the way in which various engineering disciplines affect the design, development and deployment of UAS. The fourth section assesses the future challenges and opportunities of UAS.
Technological innovation and increasingly diverse applications are two key drivers of the rapid expansion of UAS technology. The global defence budget for UAS procurement is expanding, and in the future the market for civilian UAVs is expected to outmatch that of the military. Agriculture, meteorology, conservation and border control are just a few of the diverse areas in which UAVs are making a significant impact; the author addresses all of these applications, looking at the roles and technology behind both fixed wing and rotorcraft UAVs.
Leading aeronautical consultant Reg Austin co-founded the Bristol International Remotely Piloted Vehicle (RPV) conferences in 1979, which are now the longest-established UAS conferences worldwide. In addition, Austin has over 40 years' experience in the design and development of UAS. One of Austin's programmes, the "Sprite UAV System" has been deployed around the world and operated by day and night, in all weathers.
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Morphing Aerospace Vehicles and Structures
by Various Authors
Part 57 of the Aerospace series
Morphing Aerospace Vehicles and Structures provides a highly timely presentation of the state-of-the-art, future directions and technical requirements of morphing aircraft. Divided into three sections it addresses morphing aircraft, bio-inspiration, and smart structures with specific focus on the flight control, aerodynamics, bio-mechanics, materials, and structures of these vehicles as well as power requirements and the use of advanced piezo materials and smart actuators. The tutorial approach adopted by the contributors, including underlying concepts and mathematical formulations, unifies the methodologies and tools required to provide practicing engineers and applied researchers with the insight to synthesize morphing air vehicles and morphing structures, as well as offering direction for future research.
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Sense and Avoid in UAS
Research and Applications
by Various Authors
Part 62 of the Aerospace series
There is increasing interest in the potential of UAV (Unmanned Aerial Vehicle) and MAV (Micro Air Vehicle) technology and their wide ranging applications including defense missions, reconnaissance and surveillance, border patrol, disaster zone assessment and atmospheric research. High investment levels from the military sector globally is driving research and development and increasing the viability of autonomous platforms as replacements for the remotely piloted vehicles more commonly in use.
UAV/UAS pose a number of new challenges, with the autonomy and in particular collision avoidance, detect and avoid, or sense and avoid, as the most challenging one, involving both regulatory and technical issues.
Sense and Avoid in UAS: Research and Applications covers the problem of detect, sense and avoid in UAS (Unmanned Aircraft Systems) in depth and combines the theoretical and application results by leading academics and researchers from industry and academia.
Key features:
• Presents a holistic view of the sense and avoid problem in the wider application of autonomous systems
• Includes information on human factors, regulatory issues and navigation, control, aerodynamics and physics aspects of the sense and avoid problem in UAS
• Provides professional, scientific and reliable content that is easy to understand, and
• Includes contributions from leading engineers and researchers in the field Sense and Avoid in UAS: Research and Applications is an invaluable source of original and specialised information. It acts as a reference manual for practising engineers and advanced theoretical researchers and also forms a useful resource for younger engineers and postgraduate students. With its credible sources and thorough review process, Sense and Avoid in UAS: Research and Applications provides a reliable source of information in an area that is fast expanding but scarcely covered.
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Theory of Lift
Introductory Computational Aerodynamics in MATLAB/Octave
by G. D. Mcbain
Part 66 of the Aerospace series
Starting from a basic knowledge of mathematics and mechanics gained in standard foundation classes, Theory of Lift: Introductory Computational Aerodynamics in MATLAB/Octave takes the reader conceptually through from the fundamental mechanics of lift to the stage of actually being able to make practical calculations and predictions of the coefficient of lift for realistic wing profile and planform geometries.
The classical framework and methods of aerodynamics are covered in detail and the reader is shown how they may be used to develop simple yet powerful MATLAB or Octave programs that accurately predict and visualise the dynamics of real wing shapes, using lumped vortex, panel, and vortex lattice methods.
This book contains all the mathematical development and formulae required in standard incompressible aerodynamics as well as dozens of small but complete working programs which can be put to use immediately using either the popular MATLAB or free Octave computional modelling packages.
Key features:
• Synthesizes the classical foundations of aerodynamics with hands-on computation, emphasizing interactivity and visualization.
Theory of Lift: Introductory Computational Aerodynamics in MATLAB/Octave is an introductory text for graduate and senior undergraduate students on aeronautical and aerospace engineering courses and also forms a valuable reference for engineers and designers.
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Remotely Piloted Aircraft Systems
A Human Systems Integration Perspective
by Various Authors
Part of the Aerospace series
Highlights the human components of Remotely Piloted Aircraft Systems, their interactions with the technology and each other, and the implications of human capabilities and limitations for the larger system.
• Considers human factors issues associated with RPAS, but within the context of a very large system of people, other vehicles, policy, safety concerns, and varying applications
• Chapters have been contributed by world class experts in HSI and those with operational RPAS experience
• Considers unintended consequences associated with taking a more myopic view of this system
• Examines implications for practice, policy, and research
• Considers both civil and military aspects of RPAS
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Adaptive Aeroservoelastic Control
by Ashish Tewari
Part of the Aerospace series
This is the first book on adaptive aeroservoelasticity and it presents the nonlinear and recursive techniques for adaptively controlling the uncertain aeroelastic dynamics
• Covers both linear and nonlinear control methods in a comprehensive manner
• Mathematical presentation of adaptive control concepts is rigorous
• Several novel applications of adaptive control presented here are not to be found in other literature on the topic
• Many realistic design examples are covered, ranging from adaptive flutter suppression of wings to the adaptive control of transonic limit-cycle oscillations
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Design and Analysis of Composite Structures
With Applications to Aerospace Structures
by Christos Kassapoglou
Part of the Aerospace series
New edition updated with additional exercises and two new chapters.
Design and Analysis of Composite Structures: With Applications to Aerospace Structures, 2nd Edition builds on the first edition and includes two new chapters on composite fittings and the design of a composite panel, as well additional exercises. The book enables graduate students and engineers to generate meaningful and robust designs of complex composite structures. A compilation of analysis and design methods for structural components made of advanced composites, it begins with simple parts such as skins and stiffeners and progresses through to applications such as entire components of fuselages and wings. It provides a link between theory and day-to-day design practice, using theory to derive solutions that are applicable to specific structures and structural details used in industry.
Starting with the basic mathematical derivation followed by simplifications used in real-world design,Design and Analysis of Composite Structures: With Applications to Aerospace Structures, 2nd Edition presents the level of accuracy and range of applicability of each method along with design guidelines derived from experience combined with analysis. The author solves in detail examples taken from actual applications to show how the concepts can be applied, solving the same design problem with different methods based on different drivers (e.g. cost or weight) to show how the final configuration changes as the requirements and approach change. Each chapter is followed by exercises that represent specific design problems often encountered in the aerospace industry but which are also applicable in the in the automotive, marine, and construction industries.
• Updated to include additional exercises, that represent real design problems encountered in the aerospace industry, but which are also applicable in the in the automotive, marine, and construction industries.
• Includes two new chapters. One on composite fittings and another on application and the design of a composite panel.
• Provides a toolkit of analysis and design methods that enable engineers and graduate students to generate meaningful and robust designs of complex composite structures.
• Provides solutions that can be used in optimization schemes without having to run finite element models at each iteration; thus speeding up the design process and allowing the examination of many more alternatives than traditional approaches.
• Supported by a complete set of lecture slides and solutions to the exercises hosted on a companion website for instructors.
An invaluable resource for Engineers and graduate students in aerospace engineering as well as Graduate students and engineers in mechanical, civil and marine engineering.
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Aircraft Systems
A Design and Development Guide
by Craig Lawson
Part of the Aerospace series
In-depth reference on fixed wing aircraft electrical and mechanical systems, covering electronics, hydraulics, and other essential components
Aircraft Systems delivers comprehensive material on the design and development of fixed wing aircraft electrical and mechanical systems, providing broad coverage of aircraft systems including electronics, hydraulics, pneumatics, flight control actuation, and landing gear. The book features many practical examples of existing commercial and military aircraft. Academic design studies and methods are presented, along with information on technical and mathematical methods of design. The book also features design guides for each system, including equations where appropriate to size sub-systems and major components, and discusses environmental concerns.
Topics discussed in Aircraft Systems include:
• Aircraft systems design philosophy and safety, covering systems design approaches, safety assessments, requirement captures, and component reliability
• Secondary power sources including main engines, auxiliary and ground power units, batteries, ram air turbines, and fuel cells
• Hydraulic system components, covering hydraulic fluids, pumps, and piping, reservoirs, filters, accumulators, and relief valves
• Aircraft icing and rain protection, covering ice protection systems such as electro-impulse de-icing and chemical ice protection systems
Aircraft Systems is an essential resource for undergraduate and postgraduate students studying the design of fixed wing aircraft systems. The book is also valuable to professionals in aerospace engineering due to its broad view of aircraft systems development and integration.
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Sustainable Aviation Technology and Operations
Research and Innovation Perspectives
by Various Authors
Part of the Aerospace series
Sustainable Aviation Technology and Operations
Comprehensively covers research and development initiatives to enhance the environmental sustainability of the??aviation sector
Sustainable Aviation Technology and Operations provides a comprehensive and timely outlook of recent research advances in aeronautics and air transport, with emphasis on both long-term sustainable development goals and current achievements.
This book discusses some of the most promising advances in aircraft technologies, air traffic management and systems engineering methodologies for sustainable aviation. The topics covered include: propulsion, aerodynamics, avionics, structures, materials, airspace management, biofuels and sustainable lifecycle management. The physical processes associated with various aircraft emissions - including air pollutants, noise and contrails - are presented to support the development of computational models for aircraft design, flight path optimization and environmental impact assessment. Relevant advances in systems engineering and lifecycle management processes are also covered, bridging some of the existing gaps between academic research and industry best practices. A collection of research case studies complements the book, highlighting opportunities for a timely uptake of the most promising technologies, towards a more efficient and environmentally sustainable aviation future.
Key features:
• Contains important research and industry relevant contributions from world-class experts.
• Addresses recent advances in aviation sustainability including multidisciplinary design approaches and multi-objective operational optimisation methods.
• Includes a number of research case studies, addressing propulsion, aerostructures, alternative aviation fuels, avionics, air traffic management, and sustainable lifecycle management solutions.
Sustainable Aviation Technology and Operations is an excellent book for aerospace engineers, aviation scientists, researchers and graduate students involved in the field.
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Small Unmanned Fixed-Wing Aircraft Design
A Practical Approach
by Andrew J. Keane
Part of the Aerospace series
“Small Unmanned Fixed-wing Aircraft Design” is the essential guide to designing, building and testing fixed wing UAVs (or drones). It deals with aircraft from two to 150 kg in weight and is based on the first-hand experiences of the world-renowned UAV team at the UK's University of Southampton.
The book covers both the practical aspects of designing, manufacturing and flight testing and outlines and the essential calculations needed to underpin successful designs. It describes the entire process of UAV design from requirements definition to configuration layout and sizing, through preliminary design and analysis using simple panel codes and spreadsheets to full CFD and FEA models and on to detailed design with parametric CAD tools. Its focus is on modest cost approaches that draw heavily on the latest digital design and manufacturing methods, including a strong emphasis on utilizing off-the-shelf components, low cost analysis, automated geometry modelling and 3D printing.
It deliberately avoids a deep theoretical coverage of aerodynamics or structural mechanics; rather it provides a design team with sufficient insights and guidance to get the essentials undertaken more pragmatically. The book contains many all-colour illustrations of the dozens of aircraft built by the authors and their students over the last ten years giving much detailed information on what works best. It is predominantly aimed at under-graduate and MSc level student design and build projects, but will be of interest to anyone engaged in the practical problems of getting quite complex unmanned aircraft flying. It should also appeal to the more sophisticated aero-modeller and those engaged on research based around fixed wing UAVs.
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Introduction to Nonlinear Aeroelasticity
by Grigorios Dimitriadis
Part of the Aerospace series
Introduces the latest developments and technologies in the area of nonlinear aeroelasticity.
Nonlinear aeroelasticity has become an increasingly popular research area in recent years. There have been many driving forces behind this development, increasingly flexible structures, nonlinear control laws, materials with nonlinear characteristics, etc. Introduction to Nonlinear Aeroelasticity covers the theoretical basics in nonlinear aeroelasticity and applies the theory to practical problems.
As nonlinear aeroelasticity is a combined topic, necessitating expertise from different areas, the book introduces methodologies from a variety of disciplines such as nonlinear dynamics, bifurcation analysis, unsteady aerodynamics, non-smooth systems and others. The emphasis throughout is on the practical application of the theories and methods, so as to enable the reader to apply their newly acquired knowledge.
Key features:
• Covers the major topics in nonlinear aeroelasticity, from the galloping of cables to supersonic panel flutter.
• Discusses nonlinear dynamics, bifurcation analysis, numerical continuation, unsteady aerodynamics and non-smooth systems.
• Considers the practical application of the theories and methods.
• Covers nonlinear dynamics, bifurcation analysis and numerical methods.
• Accompanied by a website hosting Matlab code.
Introduction to Nonlinear Aeroelasticity is a comprehensive reference for researchers and workers in industry and is also a useful introduction to the subject for graduate and undergraduate students across engineering disciplines.
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Hypersonic Slender Body Aerodynamics
by Ethirajan Rathakrishnan
Part of the Aerospace series
One-of-a-kind resource on theoretical and application aspects of hypersonic slender body aerodynamics with many didactic features included throughout
Developed using class-tested course material, Hypersonic Slender Body Aerodynamics presents the theoretical and application aspects of the subject in a precise, concise, and student-friendly manner. The text includes a large number of worked examples, figures, diagrams, tables, and exercise problems.
This book covers the subject material beginning from the definition of the slender body geometry through to the study of flow field around the body and the calculation of the aerodynamic and thermal loads acting on the body at speeds ranging from low to high (i.e., from incompressible to hypersonic speeds). The Mach number independence principle and approximate theories for caret wings are also covered, among many other key topics.
This book is unique in its comprehensive coverage of the topic, enabling readers to find information in one place instead of scattered throughout proprietary wind tunnel test data, flight test data, government technical reports, scientific literature sources, and numerical methods.
Some of the concepts explored in Hypersonic Slender Body Aerodynamics include:
• Wings of supersonic aircraft, covering sharp leading edges and ground and viscous effects, and pressure distribution on surfaces, covering transverse and longitudinal flow
• Hypersonic aerodynamics, covering atmospheric properties, hypersonic-flow characteristics, governing equations, and flow past a semi-wedge
• Application of slender-body theory, covering leading-edge heat transfer, sublimation, aerodynamic effects, nose bluntness, blast-wave theory, and thin shock layers
• Axisymmetric slender bodies, covering potential flow solutions and pressure distribution, and drag of slender bodies, covering shape factor and blunt after-body corrections
Skillfully written with a clear and engaging writing style, Hypersonic Slender Body Aerodynamics is an essential learning resource on the subject for undergraduate and graduate students of aerospace engineering and practicing engineers working in aerospace research labs and industries. It is a perfect textbook for courses on slender body aerodynamics.
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Aircraft Performance
Theory and Practice for Pilots
by Peter J. Swatton
Part of the Aerospace series
Aircraft Performance Theory and Practice for Pilots, 2ndEditionaddresses both European aircraft performance requirements (CS-23 and CS-25) and the Joint Aviation Regulations Operations rules (JAR-OPS 1) and so provides comprehensive and up to date coverage of the complex conditions within which all European public transport aeroplanes must operate today.
The subject of aircraft performance is an important part of the JAA Flight Crew Licensing syllabus for the examinations for commercial and airline transport licences, and this book provides a clear and authoritative text on a difficult topic.
It will also be of interest to commercial pilots for their annual standardization test and to flight planners, operations staff and airport operators.
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Unsteady Aerodynamics
Potential and Vortex Methods
by Grigorios Dimitriadis
Part of the Aerospace series
Unsteady Aerodynamics
A comprehensive overview of unsteady aerodynamics and its applications
The study of unsteady aerodynamics goes back a century and has only become more significant as aircraft become increasingly sophisticated, fly faster, and their structures are lighter and more flexible. Progress in the understanding of flow physics, computing power and techniques, and modelling technologies has led to corresponding progress in unsteady aerodynamics, with a wide range of methods currently used to predict the performance of engineering structures under unsteady conditions.
Unsteady Aerodynamics offers a comprehensive and systematic overview of the application of potential and vortex methods to the subject. Beginning with an introduction to the fundamentals of unsteady flow, it then discusses the modelling of attached and separated, incompressible and compressible flows around two-dimensional and three-dimensional bodies. The result is an essential resource for design and simulation in aerospace engineering.
Unsteady Aerodynamics readers will also find:
• MATLAB examples and exercises throughout, with codes and solutions on an accompanying website
• Detailed discussion of most classes of unsteady phenomena, including flapping flight, transonic flow, dynamic stall, flow around bluff bodies and more
• Validation of theoretical and numerical predictions using comparisons to experimental data from the literature
Unsteady Aerodynamics is ideal for researchers, engineers, and advanced students in aerospace engineering.
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Computational Modelling and Simulation of Aircraft and the Environment, Volume 2
Aircraft Dynamics
by Dominic J. Diston
Part of the Aerospace series
Computational Modelling and Simulation of Aircraft and the Environment
An in-depth discussion of aircraft dynamics modelling and simulation
This book provides a comprehensive guide to modelling and simulation from basic physical and mathematical principles, giving the reader sufficient information to be able to build computational models of aircraft for the purposes of simulation and evaluation. Highly relevant to practitioners, it takes into account the multi-disciplinary nature of aerospace products and the integrated nature of the models needed in order to represent them. Volume 1- Platform Kinematics and Synthetic Environment focused on the modelling of a synthetic environment in which aircraft operate and its spatial relationship with vehicles that are situated and moving within it. This volume focuses on the modelling of aircraft and the interpretation of their flight dynamics.
Key features:
• Includes chapters on equations of motion, fixed-wing aerodynamics, longitudinal flight and gas turbines, as well as an opening chapter that presents an overview of flight modelling and a concluding chapter that presents a number of additional topics such as aircraft structures and embedded systems.
• Serves as both a student text and practitioner reference.
• Follows on from previous Aerospace Series titles, offering a complementary view of vehicles and systems from the perspectives of mathematics, physics and simulation.
This book offers a comprehensive guide for senior, graduate and postgraduate students of aerospace engineering as well as professional engineers involved in the modelling and simulation of aircraft.
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Flight Simulation Software
Design, Development and Testing
by David Allerton
Part of the Aerospace series
Flight Simulation Software
Explains the many aspects of flight simulator design, including open-source tools for developing an engineering flight simulator.
Flight simulation is an indispensable technology for civil and military aviation and the aerospace industry. Real-time simulation tools span across all aspects of aircraft development, from aerodynamics and flight dynamics to avionics and image generation systems. Knowledge of flight simulation software is vital for aerospace engineering professionals, educators, and students. Flight Simulation Software contains comprehensive and up-to-date coverage of the computer tools required to design and develop a flight simulator.
Written by a noted expert with decades of experience developing flight simulators in academia, this highly practical resource enables readers to develop their own simulations with readily available open-source software rather than relying on costly commercial simulation packages. The book features working software taken from operational flight simulators and provides step-by-step guidance on software design, computer graphics, parallel processing, aircraft equations of motion, navigation and flight control systems, and more.
• Explains both fundamental theory and real-world practice of simulation in engineering design
• Covers a wide range of topics, including coding standards, software validation, user interface design, and sensor modelling
• Describes techniques used in modern flight simulation including distributed architectures and the use of GPUs for real-time graphics rendering
• Addresses unique aspects of flight simulation such as designing flight control systems, visual systems, and simulator instructor stations
“Flight Simulation Software” is a must-have guide for all developers and users of simulation tools, as well as the ideal textbook for relevant undergraduate and postgraduate courses in computer science, aeronautical engineering, electrical engineering, and mechanical engineering programs.
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System Health Management
With Aerospace Applications
by Various Authors
Part of the Aerospace series
“System Health Management: with Aerospace Applications” provides the first complete reference text for System Health Management (SHM), the set of technologies and processes used to improve system dependability. Edited by a team of engineers and consultants with SHM design, development, and research experience from NASA, industry, and academia, each heading up sections in their own areas of expertise and co-coordinating contributions from leading experts, the book collates together in one text the state-of-the-art in SHM research, technology, and applications. It has been written primarily as a reference text for practitioners, for those in related disciplines, and for graduate students in aerospace or systems engineering.
There are many technologies involved in SHM and no single person can be an expert in all aspects of the discipline.
“System Health Management: with Aerospace Applications” provides an introduction to the major technologies, issues, and references in these disparate but related SHM areas. Since SHM has evolved most rapidly in aerospace, the various applications described in this book are taken primarily from the aerospace industry. However, the theories, techniques, and technologies discussed are applicable to many engineering disciplines and application areas.
Readers will find sections on the basic theories and concepts of SHM, how it is applied in the system life cycle (architecture, design, verification and validation, etc.), the most important methods used (reliability, quality assurance, diagnostics, prognostics, etc.), and how SHM is applied in operations (commercial aircraft, launch operations, logistics, etc.), to subsystems (electrical power, structures, flight controls, etc.) and to system applications (robotic spacecraft, tactical missiles, rotorcraft, etc.).
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Space Flight Dynamics
by Craig A. Kluever
Part of the Aerospace series
Thorough coverage of space flight topics with self-contained chapters serving a variety of courses in orbital mechanics, spacecraft dynamics, and astronautics
This concise yet comprehensive book on space flight dynamics addresses all phases of a space mission: getting to space (launch trajectories), satellite motion in space (orbital motion, orbit transfers, attitude dynamics), and returning from space (entry flight mechanics). It focuses on orbital mechanics with emphasis on two-body motion, orbit determination, and orbital maneuvers with applications in Earth-centered missions and interplanetary missions.
“Space Flight Dynamics” presents wide-ranging information on a host of topics not always covered in competing books. It discusses relative motion, entry flight mechanics, low-thrust transfers, rocket propulsion fundamentals, attitude dynamics, and attitude control. The book is filled with illustrated concepts and real-world examples drawn from the space industry. Additionally, the book includes a "computational toolbox" composed of MATLAB M-files for performing space mission analysis.
Key features:
• Provides practical, real-world examples illustrating key concepts throughout the book
• Accompanied by a website containing MATLAB M-files for conducting space mission analysis
• Presents numerous space flight topics absent in competing titles
“Space Flight Dynamics” is a welcome addition to the field, ideally suited for upper-level undergraduate and graduate students studying aerospace engineering.
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UAS Integration Into Civil Airspace
Policy, Regulations and Strategy
by Douglas M. Marshall
Part of the Aerospace series
UAS Integration into Civil Airspace
Explores current Unmanned Air Systems policies with a view to developing a common airspace access and integration strategy
UAS Integration into Civil Airspace: Policy, Regulations and Strategy examines the current state of Unmanned Aerial Systems (UAS) airspace access and integration around the world, focusing on the efforts that have produced a regulatory response to the demand for access. This analysis discusses the proposed architectures for a common strategic and analytical thread that may serve as templates for the entire community, as well as for regulators and policymakers who must balance the needs and demands of UAS users with the general public's right to safe skies and privacy. An understanding of the market forces and business cases that are fueling the development of the technology is also covered with a focus on the economics of the industry.
The book presents a strategy for airspace access and integration that will facilitate humanitarian, environmental, social and security uses of unmanned aircraft systems on a global scale.
Key features:
• Discusses existing and evolving policies and regulations from nations around the world for operating Unmanned Aerial Systems (UAS) in civil airspace
• Examines the current status of technological developments such as UTM and U-space and explores the technological potential in the years to come
• Presents a comprehensive airspace integration strategy that balances the many conflicting interests in the UAS world, with due regard for safety, utility and affordability
UAS Integration into Civil Airspace: Policy, Regulations and Strategy is essential reading for all professionals involved in UAS industry, as well as students in mechanical engineering and law.
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Future Propulsion Systems and Energy Sources in Sustainable Aviation
by Saeed Farokhi
Part of the Aerospace series
A comprehensive review of the science and engineering behind future propulsion systems and energy sources in sustainable aviation.
“Future Propulsion Systems and Energy Sources in Sustainable Aviation” is a comprehensive reference that offers a review of the science and engineering principles that underpin the concepts of propulsion systems and energy sources in sustainable air transportation. The author, a noted expert in the field, examines the impact of air transportation on the environment and reviews alternative jet fuels, hybrid-electric and nuclear propulsion and power. He also explores modern propulsion for transonic and supersonic-hypersonic aircraft and the impact of propulsion on aircraft design.
Climate change is the main driver for the new technology development in sustainable air transportation. The book contains critical review of gas turbine propulsion and aircraft aerodynamics; followed by an insightful presentation of the aviation impact on environment. Future fuels and energy sources are introduced in a separate chapter. Promising technologies in propulsion and energy sources are identified leading to pathways to sustainable aviation. To facilitate the utility of the subject, the book is accompanied by a website that contains illustrations, and equation files. This important book:
• Contains a comprehensive reference to the science and engineering behind propulsion and power in sustainable air transportation
• Examines the impact of air transportation on the environment
• Covers alternative jet fuels and hybrid-electric propulsion and power
• Discusses modern propulsion for transonic, supersonic and hypersonic aircraft
• Examines the impact of propulsion system integration on aircraft design
Written for engineers, graduate and senior undergraduate students in mechanical and aerospace engineering, “Future Propulsion Systems and Energy Sources in Sustainable Aviation” explores the future of aviation with a guide to sustainable air transportation that includes alternative jet fuels, hybrid-electric propulsion, all-electric and nuclear propulsion.
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Introduction to Flight Testing
by James W. Gregory
Part of the Aerospace series
“Introduction to Flight Testing” provides a concise introduction to the basic flight testing methods employed on general aviation aircraft and unmanned aerial vehicles for courses in aeronautical engineering. There is particular emphasis on the use of modern on-board instruments and inexpensive, off-the-shelf portable devices that make flight testing accessible to nearly any student.
This text presents a clear articulation of standard methods for measuring aircraft performance characteristics. Topics covered include aircraft and instruments, digital data acquisition techniques, flight test planning, the standard atmosphere, uncertainty analysis, level flight performance, airspeed calibration, stall, climb and glide, take-off and landing, level turn, static and dynamic longitudinal stability, lateral-directional stability, and flight testing of unmanned aircraft systems.
Unique to this book is a detailed discussion of digital data acquisition (DAQ) techniques, which are an integral part of modern flight test programs. This treatment includes discussion of the analog-to-digital conversion, sample rate, aliasing, and filtering. These critical details provide the flight test engineer with the insight needed to understand the capabilities and limitations of digital DAQ.
Key features:
• Provides an introduction to the basic flight-testing methods and instrumentation employed on general aviation aircraft and unmanned aerial vehicles.
• Includes examples of flight testing on general aviation aircraft such as Cirrus, Diamond, and Cessna aircraft, along with unmanned aircraft vehicles.
• Suitable for courses on Aircraft Flight Test Engineering.
“Introduction to Flight Testing” provides resources and guidance for practitioners in the rapidly-developing field of drone performance flight test and the general aviation flight test community.
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Military Avionics Systems
by Ian Moir
Part of the Aerospace series
Ian Moir and Allan Seabridge
Military avionics is a complex and technically challenging field which requires a high level of competence from all those involved in the aircraft design and maintenance. As the various systems on board an aircraft evolve to become more and more inter-dependent and integrated, it is becoming increasingly important for designers to have a holistic view and knowledge of aircraft systems in order to produce an effective design for their individual components and effectively combine the systems involved.
This book introduces the military roles expected of aircraft types and describes the avionics systems required to fulfil these roles. These range from technology and architectures through to navigations systems, sensors, computing architectures and the human-machine interface. It enables students to put together combinations of systems in order to perform specific military roles.
• Sister volume to the authors' previous successful title 'Civil Avionics Systems'
• Covers a wide range of military aircraft roles and systems applications
• Offers clear and concise system descriptions
• Includes case studies and examples from current projects
• Features full colour illustrations detailing aircraft display systems
“Military Avionics Systems” will appeal to practitioners in the aerospace industry across many disciplines such as aerospace engineers, designers, pilots, aircrew, maintenance engineers, ground crew, navigation experts, weapons developers and instrumentation developers. It also provides a valuable reference source to students in the fields of systems and aerospace engineering and avionics.
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Aircraft Control Allocation
by Wayne Durham
Part of the Aerospace series
An authoritative work on aircraft control allocation by its pioneers
“Aircraft Control Allocation” addresses the problem of allocating supposed redundant flight controls. It provides introductory material on flight dynamics and control to provide the context, and then describes in detail the geometry of the problem. The book includes a large section on solution methods, including 'Banks' method', a previously unpublished procedure. Generalized inverses are also discussed at length. There is an introductory section on linear programming solutions, as well as an extensive and comprehensive appendix dedicated to linear programming formulations and solutions. Discrete-time, or frame-wise allocation, is presented, including rate-limiting, nonlinear data, and preferred solutions.
Key features:
• Written by pioneers in the field of control allocation.
• Comprehensive explanation and discussion of the major control allocation solution methods.
• Extensive treatment of linear programming solutions to control allocation.
• A companion web site contains the code of a MATLAB/Simulink flight simulation with modules that incorporate all of the major solution methods.
• Includes examples based on actual aircraft.
The book is a vital reference for researchers and practitioners working in aircraft control, as well as graduate students in aerospace engineering.
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Advanced UAV Aerodynamics, Flight Stability and Control
Novel Concepts, Theory and Applications
by Various Authors
Part of the Aerospace series
Comprehensively covers emerging aerospace technologies.
Advanced UAV aerodynamics, flight stability and control: Novel concepts, theory and applications presents emerging aerospace technologies in the rapidly growing field of unmanned aircraft engineering. Leading scientists, researchers and inventors describe the findings and innovations accomplished in current research programs and industry applications throughout the world. Topics included cover a wide range of new aerodynamics concepts and their applications for real world fixed-wing (airplanes), rotary wing (helicopter) and quad-rotor aircraft.
The book begins with two introductory chapters that address fundamental principles of aerodynamics and flight stability and form a knowledge base for the student of Aerospace Engineering. The book then covers aerodynamics of fixed wing, rotary wing and hybrid unmanned aircraft, before introducing aspects of aircraft flight stability and control.
Key features:
• Sound technical level and inclusion of high-quality experimental and numerical data.
• Direct application of the aerodynamic technologies and flight stability and control principles described in the book in the development of real-world novel unmanned aircraft concepts.
• Written by world-class academics, engineers, researchers and inventors from prestigious institutions and industry.
The book provides up-to-date information in the field of Aerospace Engineering for university students and lecturers, aerodynamics researchers, aerospace engineers, aircraft designers and manufacturers.
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Differential Game Theory With Applications to Missiles and Autonomous Systems Guidance
by Farhan A. Faruqi
Part of the Aerospace series
“Differential Game Theory with Applications to Missiles and Autonomous Systems” explains the use of differential game theory in autonomous guidance and control systems.
The book begins with an introduction to the basic principles before considering optimum control and game theory. Two-party and multi-party game theory and guidance are then covered and, finally, the theory is demonstrated through simulation examples and models and the simulation results are discussed. Recent developments in the area of guidance and autonomous systems are also presented.
Key features:
• Presents new developments and how they relate to established control systems knowledge.
• Demonstrates the theory through simulation examples and models.
• Covers two-party and multi-party game theory and guidance.
• Accompanied by a website hosting MATLAB® code.
The book is essential reading for researchers and practitioners in the aerospace and defence industries as well as graduate students in aerospace engineering.
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Civil Avionics Systems
by Ian Moir
Part of the Aerospace series
“Civil Avionics Systems”, Second Edition, is an updated and in-depth practical guide to integrated avionic systems as applied to civil aircraft and this new edition has been expanded to include the latest developments in modern avionics. It describes avionic systems and potential developments in the field to help educate students and practitioners in the process of designing, building and operating modern aircraft in the contemporary aviation system.
Integration is a predominant theme of this book, as aircraft systems are becoming more integrated and complex, but so is the economic, political and technical environment in which they operate.
Key features:
• Content is based on many years of practical industrial experience by the authors on a range of civil and military projects
• Generates an understanding of the integration and interconnectedness of systems in modern complex aircraft
• Updated contents in the light of latest applications
• Substantial new material has been included in the areas of avionics technology, software and system safety
The authors are all recognised experts in the field and between them have over 140 years' experience in the aircraft industry. Their direct and accessible style ensures that “Civil Avionics Systems”, Second Edition is a must-have guide to integrated avionic systems in modern aircraft for those in the aerospace industry and academia.
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Advanced Aircraft Design
Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes
by Egbert Torenbeek
Part of the Aerospace series
Although the overall appearance of modern airliners has not changed a lot since the introduction of jetliners in the 1950s, their safety, efficiency and environmental friendliness have improved considerably. Main contributors to this have been gas turbine engine technology, advanced materials, computational aerodynamics, advanced structural analysis and on-board systems. Since aircraft design became a highly multidisciplinary activity, the development of multidisciplinary optimization (MDO) has become a popular new discipline. Despite this, the application of MDO during the conceptual design phase is not yet widespread.
Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes presents a quasi-analytical optimization approach based on a concise set of sizing equations. Objectives are aerodynamic efficiency, mission fuel, empty weight and maximum takeoff weight. Independent design variables studied include design cruise altitude, wing area and span and thrust or power loading. Principal features of integrated concepts such as the blended wing and body and highly non-planar wings are also covered.
The quasi-analytical approach enables designers to compare the results of high-fidelity MDO optimization with lower-fidelity methods which need far less computational effort. Another advantage to this approach is that it can provide answers to "what if" questions rapidly and with little computational cost.
Key features:
• Presents a new fundamental vision on conceptual airplane design optimization
• Provides an overview of advanced technologies for propulsion and reducing aerodynamic drag
• Offers insight into the derivation of design sensitivity information
• Emphasizes design based on first principles
• Considers pros and cons of innovative configurations
• Reconsiders optimum cruise performance at transonic Mach numbers
Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes advances understanding of the initial optimization of civil airplanes and is a must-have reference for aerospace engineering students, applied researchers, aircraft design engineers and analysts.
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Aircraft Systems Integration of Air-Launched Weapons
by Keith A. Rigby
Part of the Aerospace series
From the earliest days of aviation where the pilot would drop simple bombs by hand, to the highly agile, stealthy aircraft of today that can deliver smart ordnance with extreme accuracy, engineers have striven to develop the capability to deliver weapons against targets reliably, safely and with precision.
“Aircraft Systems Integration of Air-Launched Weapons” introduces the various aspects of weapons integration, primarily from the aircraft systems integration viewpoint, but also considers key parts of the weapon and the desired interactions with the aircraft required for successful target engagement.
Key features:
• Addresses the broad range of subjects that relate directly to the systems integration of air-launched weapons with aircraft, such as the integration process, system and subsystem architectures, the essential contribution that open, international standards have on improving interoperability and reducing integration costs and timescales
• Describes the recent history of how industry and bodies such as NATO have driven the need for greater interoperability between weapons and aircraft and worked to reduce the cost and timescales associated with the systems integration of complex air-launched weapons with aircraft
• Explores future initiatives and technologies relating to the reduction of systems integration costs and timescales
The systems integration of air-launched weapons with aircraft requires a multi-disciplinary set of engineering capabilities. As a typical weapons integration life-cycle spans several years, new engineers have to learn the skills required by on-the-job training and working with experienced weapons integrators. Aircraft Systems Integration of Air-Launched Weapons augments hands-on experience, thereby enabling the development of subject matter expertise more quickly and in a broader context than would be achieved by working through the life-cycle on one specific project. This book also serves as a useful revision source for experienced engineers in the field.
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Aircraft Aerodynamic Design
Geometry and Optimization
by András Sóbester
Part of the Aerospace series
Optimal aircraft design is impossible without a parametric representation of the geometry of the airframe. We need a mathematical model equipped with a set of controls, or design variables, which generates different candidate airframe shapes in response to changes in the values of these variables. This model's objectives are to be flexible and concise, and capable of yielding a wide range of shapes with a minimum number of design variables. Moreover, the process of converting these variables into aircraft geometries must be robust. Alas, flexibility, conciseness and robustness can seldom be achieved simultaneously.
Aircraft Aerodynamic Design: Geometry and Optimization addresses this problem by navigating the subtle trade-offs between the competing objectives of geometry parameterization. It beginswith the fundamentals of geometry-centred aircraft design, followed by a review of the building blocks of computational geometries, the curve and surface formulations at the heart of aircraft geometry. The authors then cover a range of legacy formulations in the build-up towards a discussion of the most flexible shape models used in aerodynamic design (with a focus on lift generating surfaces). The book takes a practical approach and includes MATLAB®, Python and Rhinoceros® code, as well as 'real-life' example case studies.
Key features:
• Covers effective geometry parameterization within the context of design optimization
• Demonstrates how geometry parameterization is an important element of modern aircraft design
• Includes code and case studies which enable the reader to apply each theoretical concept either as an aid to understanding or as a building block of their own geometry model
• Accompanied by a website hosting codes
Aircraft Aerodynamic Design: Geometry and Optimization is a practical guide for researchers and practitioners in the aerospace industry, and a reference for graduate and undergraduate students in aircraft design and multidisciplinary design optimization.
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Introduction to Aircraft Aeroelasticity and Loads
by Jan R. Wright
Part of the Aerospace series
Introduction to Aircraft Aeroelasticity and Loads, Second Edition is an updated new edition offering comprehensive coverage of the main principles of aircraft aeroelasticity and loads. For ease of reference, the book is divided into three parts and begins by reviewing the underlying disciplines of vibrations, aerodynamics, loads and control, and then goes on to describe simplified models to illustrate aeroelastic behaviour and aircraft response and loads for the flexible aircraft before introducing some more advanced methodologies. Finally, it explains how industrial certification requirements for aeroelasticity and loads may be met and relates these to the earlier theoretical approaches used.
Key features of this new edition include:
• Uses a unified simple aeroelastic model throughout the book
• Major revisions to chapters on aeroelasticity
• Updates and reorganisation of chapters involving Finite Elements
• Some reorganisation of loads material
• Updates on certification requirements
• Accompanied by a website containing a solutions manual, and MATLAB® and SIMULINK® programs that relate to the models used
Introduction to Aircraft Aeroelasticity and Loads, Second Edition is a must-have reference for researchers and practitioners working in the aeroelasticity and loads fields, and is also an excellent textbook for senior undergraduate and graduate students in aerospace engineering.
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Modeling the Effect of Damage in Composite Structures
Simplified Approaches
by Christos Kassapoglou
Part of the Aerospace series
Comprehensively covers new and existing methods for the design and analysis of composites structures with damage present.
• Provides efficient and accurate approaches for analysing structures with holes and impact damage
• Introduces a new methodology for fatigue analysis of composites
• Provides design guidelines, and step-by-step descriptions of how to apply the methods, along with evaluation of their accuracy and applicability
• Includes problems and exercises
• Accompanied by a website hosting lecture slides and solutions
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Understanding Aerodynamics
Arguing from the Real Physics
by Doug McLean
Part of the Aerospace series
Much-needed, fresh approach that brings a greater insight into the physical understanding of aerodynamics.
Based on the author's decades of industrial experience with Boeing, this book helps students and practicing engineers to gain a greater physical understanding of aerodynamics. Relying on clear physical arguments and examples, Mclean provides a much-needed, fresh approach to this sometimes-contentious subject without shying away from addressing "real" aerodynamic situations as opposed to the oversimplified ones frequently used for mathematical convenience. Motivated by the belief that engineering practice is enhanced in the long run by a robust understanding of the basics as well as real cause-and-effect relationships that lie behind the theory, he provides intuitive physical interpretations and explanations, debunking commonly-held misconceptions and misinterpretations, and building upon the contrasts provided by wrong explanations to strengthen understanding of the right ones.
• Provides a refreshing view of aerodynamics that is based on the author's decades of industrial experience yet is always tied to basic fundamentals.
• Provides intuitive physical interpretations and explanations, debunking commonly-held misconceptions and misinterpretations
• Offers new insights to some familiar topics, for example, what the Biot-Savart law really means and why it causes so much confusion, what "Reynolds number" and "incompressible flow" really mean, and a real physical explanation for how an airfoil produces lift.
• Addresses "real" aerodynamic situations as opposed to the oversimplified ones frequently used for mathematical convenience and omits mathematical details whenever the physical understanding can be conveyed without them.
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Aircraft Systems Classifications
A Guide to Key Characteristics and Requirements
by Allan Seabridge
Part of the Aerospace series
“Aircraft Systems Classifications: A Handbook of Characteristics and Design Guidelines” provides comprehensive information on aircraft systems delivered in a concise, direct, and standardized way, allowing readers to easily find the information they need. The book presents a full set of characteristics and requirements for all types of aircraft systems, including avionic, mission, and supporting ground systems, in a single volume. Readers can delve further into specific topics by referencing the detailed glossary and bibliography.
To aid in reader comprehension, each aircraft system is broken down according to various criteria, such as:
• Purpose, description, and safety
• Integration with other systems
• Key interfaces and design drivers
• Modeling and simulation
• Best practices and future trends
Written for aerospace professionals, researchers, and advanced students with some existing knowledge of the aircraft industry, this book allows readers to quickly reference information on every aspect of aircraft systems.
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Aerospace Propulsion
by T. W. Lee
Part of the Aerospace series
Aerospace propulsion devices embody some of the most advanced technologies, ranging from materials, fluid control, and heat transfer and combustion. In order to maximize the performance, sophisticated testing and computer simulation tools are developed and used.
“Aerospace Propulsion” comprehensively covers the mechanics and thermal-fluid aspects of aerospace propulsion, starting from the fundamental principles, and covering applications to gas-turbine and space propulsion (rocket) systems. It presents modern analytical methods using MATLAB and other advanced software and includes essential elements of both gas-turbine and rocket propulsion systems. Gas turbine coverage includes thermodynamic analysis, turbine components, diffusers, compressors, turbines, nozzles, compressor-turbine matching, combustors and afterburners. Rocket coverage includes chemical rockets, electrical rockets, nuclear and solar sail.
Key features:
• Both gas-turbine and rocket propulsion covered in a single volume
• Presents modern analytical methods and examples
• Combines fundamentals and applications, including space applications
• Accompanied by a website containing MATLAB examples, problem sets and solutions
“Aerospace Propulsion” is a comprehensive textbook for senior undergraduate graduate and aerospace propulsion courses, and is also an excellent reference for researchers and practicing engineers working in this area.
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Design and Development of Aircraft Systems
by Allan Seabridge
Part of the Aerospace series
Provides a significant update to the definitive book on aircraft system design.
This book is written for anyone who wants to understand how industry develops the customer requirement for aircraft into a fully integrated, tested, and qualified product that is safe to fly and fit for purpose. The new edition of Design and Development of Aircraft Systems fully expands its already comprehensive coverage to include both conventional and unmanned systems. It also updates all chapters to bring them in line with current design practice and technologies taught in courses at Cranfield, Bristol, and Loughborough universities in the UK.
“Design and Development of Aircraft Systems”, 3rd Edition begins with an introduction to the subject. It then introduces readers to the aircraft systems (airframe, vehicle, avionic, mission, and ground systems). Following that comes a chapter on the design and development process. Other chapters look at design drivers, systems architectures, systems integration, verification of system requirements, practical considerations, and configuration control. The book finishes with sections that discuss the potential impact of complexity on flight safety, key characteristics of aircraft systems, and more.
• Provides a holistic view of aircraft system design, describing the interactions among subsystems such as fuel, navigation, flight control, and more
• Substantially updated coverage of systems engineering, design drivers, systems architectures, systems integration, modelling of systems, practical considerations, and systems examples
• Incorporates essential new material on the regulatory environment for both manned and unmanned systems
• Discussion of trends towards complex systems, automation, integration and the potential for an impact on flight safety
“Design and Development of Aircraft Systems”, 3rd Edition is an excellent book for aerospace engineers, researchers, and graduate students involved in the field.
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Introduction to Aerospace Engineering With a Flight Test Perspective
by Stephen Corda
Part of the Aerospace series
Comprehensive textbook integrating the fundamentals of flight testing with introductory concepts in aerospace engineering
Introduction to Aerospace Engineering with a Flight Test Perspective provides a solid foundation in the fundamentals of aerospace engineering while illuminating many aspects of real-world flight, covering topics such as aerodynamics, propulsion, performance, and stability and control. End-of-chapter problems are included along with a solutions manual for instructors.
The Second Edition includes two new chapters, one providing a timely introduction to hypersonics and the other introducing the fundamentals of spaceflight.
Introduction to Aerospace Engineering with a Flight Test Perspective discusses topics including:
• Historical perspectives of the first flights of airplanes, rotorcraft, and spacecraft
• Introductory concepts of airplanes, rotorcraft, unmanned aerial vehicles, and lighter-than-air vehicles
• Placement of the reader in the aircraft cockpit to fly and learn the basics of flight test
• Fundamentals of subsonic, transonic, supersonic, and hypersonic flight, with explanations of the theories of lift and the generation of drag
• Types of non-airbreathing rocket propulsion, including liquid propellant rocket engines and solid rocket motors, as well as air-breathing propulsion, including propeller-driven and jet engines
• Concepts of aircraft performance in cruising, climbing, gliding, and turning flight
• Longitudinal and lateral-directional stability and control
• An introduction to hypersonic vehicles, aero-thermodynamics, and propulsion
• Orbital mechanics, covering Kepler's laws, the two-body problem, types of trajectories and orbits, and atmospheric entry
Introduction to Aerospace Engineering with a Flight Test Perspective is an excellent accompaniment to any introductory course in aerospace engineering taught at civilian universities, military academies, and test pilot schools. The text may also be used in more advanced courses in flight testing, aerodynamics, performance, and design.
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Modelling and Managing Airport Performance
by Various Authors
Part of the Aerospace series
“Modelling and Managing Airport Performance” provides an integrated view of state-of-the-art research on measuring and improving the performance of airport systems with consideration of both airside and landside operations. The considered facets of performance include capacity, delays, economic costs, noise, emissions and safety. Several of the contributions also examine policies for managing congestion and allocating sparse capacity, as well as for mitigating the externalities of noise, emissions, and safety/risk.
Key features:
• Provides a global perspective with contributing authors from Europe, North and South America with backgrounds in academia, research institutions, government, and industry
• Contributes to the definition, interpretation, and shared understanding of airport performance measures and related concepts
• Considers a broad range of measures that quantify operational and environmental performance, as well as safety and risk
• Discusses concepts and strategies for dealing with the management of airport performance
• Presents state-of-the-art modelling capabilities and identifies future modelling needs
Themed around 3 sections—Modelling Airport Performance, Assessing Airport Impacts, and Managing Airport Performance and Congestion Modelling and Managing Airport Performance is a valuable reference for researchers and practitioners in the global air transportation community.
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Scramjet Propulsion
A Practical Introduction
by Dora Musielak
Part of the Aerospace series
Scramjet Propulsion
Explore the cutting edge of HAP technologies with this comprehensive resource from an international leader in her field,
“Scramjet Propulsion: A Practical Introduction” delivers a comprehensive treatment of hypersonic air breathing propulsion and its applications. The book covers the most up-to-date hypersonic technologies, like endothermic fuels, fuel injection and flameholding systems, high temperature materials, and TPS, and offers technological overviews of hypersonic flight platforms like the X-43A, X-51A, and HiFIRE. It is organized around easy-to-understand explanations of technical challenges and provides extensive references for the information contained within.
The highly accomplished author provides readers with a fulsome description of the theoretical underpinnings of hypersonic technologies, as well as critical design and technology issues affecting hypersonic air breathing propulsion technologies. The book's combination of introductory theory and advanced instruction about individual hypersonic engine components is ideal for students and practitioners in fields as diverse as hypersonic vehicle and propulsion development for missile defense technologies, launch aerospaceplanes, and civilian transports. Over 250 illustrations and tables round out the material. Readers will also learn from:
• A thorough introduction to hypersonic flight, hypersonic vehicle concepts, and a review of fundamental principles in hypersonic air breathing propulsion
• Explorations of the aerothermodynamics of scramjet engines and the design of scramjet components, as well as hypersonic air breathing propulsion combustors and fuels
• Analyses of dual-mode combustion phenomena, materials structures, and thermal management in hypersonic vehicles, and combined cycle propulsion
• An examination of CFD analysis, ground and flight testing, and simulation
Perfect for researchers and graduate students in aerospace engineering, “Scramjet Propulsion: A Practical Introduction” is also an indispensable addition to the libraries of engineers working on hypersonic vehicle development seeking a state-of-the-art resource in one of the most potentially disruptive areas of aerospace research today.
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Essentials of Supersonic Commercial Aircraft Conceptual Design
by Egbert Torenbeek
Part of the Aerospace series
Provides comprehensive coverage of how supersonic commercial aircraft are designed
This must-have guide to conceptual supersonic aircraft design provides a state-of-the art overview of the subject, along with expert analysis and discussion. It examines the challenges of high-speed flight, covers aerodynamic phenomena in supersonic flow and aerodynamic drag in cruising flight, and discusses the advantages and disadvantages of oblique wing aircraft.
Essentials of Supersonic Commercial Aircraft Conceptual Design is intended for members of a team producing an initial design concept of an airliner with the capability of making supersonic cruising flights. It begins with a synopsis of the history of supersonic transport aircraft development and continues with a chapter on the challenges of high-speed flight, which discusses everything from top level requirements and cruise speed requirements to fuel efficiency and cruise altitude. It then covers weight sensitivity, aerodynamic phenomena in supersonic flow, thin wings in two-dimensional flow, flat wings in inviscid supersonic flow, aerodynamic drag in cruising flight, and aerodynamic efficiency of SCV configurations. The book finishes with a chapter that examines oblique wing aircraft.
• Provides supersonic aircraft designers with everything they need to know about developing current and future high speed commercial jet planes
• Examines the many challenges of high-speed flight
• Covers aerodynamic phenomena in supersonic flow and aerodynamic drag in cruising flight
• Discusses the advantages and disadvantages of oblique wing aircraft
Essentials of Supersonic Commercial Aircraft Conceptual Design is an ideal book for researchers and practitioners in the aerospace industry, as well as for graduate students in aerospace engineering.
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Helicopter Flight Dynamics
Including a Treatment of Tiltrotor Aircraft
by Gareth D. Padfield
Part of the Aerospace series
The behaviour of helicopters and tiltrotor aircraft is so complex that understanding the physical mechanisms at work in trim, stability and response, and thus the prediction of Flying Qualities, requires a framework of analytical and numerical modelling and simulation. Good Flying Qualities are vital for ensuring that mission performance is achievable with safety and, in the first and second editions of “Helicopter Flight Dynamics”, a comprehensive treatment of design criteria was presented, relating to both normal and degraded Flying Qualities. Fully embracing the consequences of Degraded Flying Qualities during the design phase will contribute positively to safety. In this third edition, two new Chapters are included. Chapter 9 takes the reader on a journey from the origins of the story of Flying Qualities, tracing key contributions to the developing maturity and to the current position. Chapter 10 provides a comprehensive treatment of the Flight Dynamics of tiltrotor aircraft; informed by research activities and the limited data on operational aircraft. Many of the unique behavioural characteristics of tiltrotors are revealed for the first time in this book.
The accurate prediction and assessment of Flying Qualities draws on the modelling and simulation discipline on the one hand and testing practice on the other. Checking predictions in flight requires clearly defined mission tasks, derived from realistic performance requirements. High fidelity simulations also form the basis for the design of stability and control augmentation systems, essential for conferring Level 1 Flying Qualities. The integrated description of flight dynamic modelling, simulation and flying qualities of rotorcraft forms the subject of this book, which will be of interest to engineers practising and honing their skills in research laboratories, academia and manufacturing industries, test pilots and flight test engineers, and as a reference for graduate and postgraduate students in aerospace engineering.
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