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Design And Development Of Aircraft Systems

Author: Ian Moir
Publisher: John Wiley & Sons
ISBN: 1118469143
Size: 48.88 MB
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Now covering both conventional and unmanned systems, this isa significant update of the definitive book on aircraft systemdesign Design and Development of Aircraft Systems, SecondEdition is for people who want to understand how industrydevelops the customer requirement into a fully integrated, tested,and qualified product that is safe to fly and fit for purpose. Thisedition has been updated to take into account the growth ofunmanned air vehicles, together with updates to all chapters tobring them in line with current design practice and technologies astaught on courses at BAE Systems and Cranfield, Bristol andLoughborough universities in the UK. Design and Development of Aircraft Systems, SecondEdition Provides a holistic view of aircraft system design describingthe interaction between all of the subsystems such as fuel system,navigation, flight control etc. Covers all aspects of design including systems engineering,design drivers, systems architectures, systems integration,modelling of systems, practical considerations, & systemsexamples. Incorporates essential new material on Unmanned AircraftSystems (UAS). Design and Development of Aircraft Systems,Second Edition has been written to be generic and not todescribe any single process. It aims to complement othervolumes in the Wiley Aerospace Series, in particular AircraftSystems, Third Edition and Civil Avionics Systems by thesame authors, and will inform readers of the work that is carriedout by engineers in the aerospace industry to produce innovativeand challenging – yet safe and reliable – systems andaircraft. Essential reading for Aerospace Engineers.

Unmanned Aircraft Systems

Author: Reg Austin
Publisher: John Wiley & Sons
ISBN: 1119964261
Size: 19.34 MB
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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.

Aircraft Flight Dynamics And Control

Author: Wayne Durham
Publisher: John Wiley & Sons
ISBN: 1118646800
Size: 39.47 MB
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Aircraft Flight Dynamics and Control addresses airplane flight dynamics and control in a largely classical manner, but with references to modern treatment throughout. Classical feedback control methods are illustrated with relevant examples, and current trends in control are presented by introductions to dynamic inversion and control allocation. This book covers the physical and mathematical fundamentals of aircraft flight dynamics as well as more advanced theory enabling a better insight into nonlinear dynamics. This leads to a useful introduction to automatic flight control and stability augmentation systems with discussion of the theory behind their design, and the limitations of the systems. The author provides a rigorous development of theory and derivations and illustrates the equations of motion in both scalar and matrix notation. Key features: Classical development and modern treatment of flight dynamics and control Detailed and rigorous exposition and examples, with illustrations Presentation of important trends in modern flight control systems Accessible introduction to control allocation based on the author's seminal work in the field Development of sensitivity analysis to determine the influential states in an airplane's response modes End of chapter problems with solutions available on an accompanying website Written by an author with experience as an engineering test pilot as well as a university professor, Aircraft Flight Dynamics and Control provides the reader with a systematic development of the insights and tools necessary for further work in related fields of flight dynamics and control. It is an ideal course textbook and is also a valuable reference for many of the necessary basic formulations of the math and science underlying flight dynamics and control.

Aircraft Systems

Author: Ian Moir
Publisher: John Wiley & Sons
ISBN: 1119965209
Size: 50.37 MB
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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.

Aircraft Design

Author: Mohammad H. Sadraey
Publisher: John Wiley & Sons
ISBN: 1118352807
Size: 52.77 MB
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A comprehensive approach to the air vehicle design processusing the principles of systems engineering Due to the high cost and the risks associated with development,complex aircraft systems have become a prime candidate for theadoption of systems engineering methodologies. This book presentsthe entire process of aircraft design based on a systemsengineering approach from conceptual design phase, through topreliminary design phase and to detail design phase. Presenting in one volume the methodologies behind aircraftdesign, this book covers the components and the issues affected bydesign procedures. The basic topics that are essential to theprocess, such as aerodynamics, flight stability andcontrol, aero-structure, and aircraft performance are reviewedin various chapters where required. Based on thesefundamentals and design requirements, the author explains thedesign process in a holistic manner to emphasise the integration ofthe individual components into the overall design. Throughout thebook the various design options are considered and weighed againsteach other, to give readers a practical understanding of theprocess overall. Readers with knowledge of the fundamental concepts ofaerodynamics, propulsion, aero-structure, and flight dynamics willfind this book ideal to progress towards the next stage in theirunderstanding of the topic. Furthermore, the broad variety ofdesign techniques covered ensures that readers have the freedom andflexibility to satisfy the design requirements when approachingreal-world projects. Key features: • Providesfull coverage of the design aspects of an air vehicle including:aeronautical concepts, design techniques and design flowcharts • Featuresend of chapter problems to reinforce the learning process as wellas fully solved design examples at component level • Includes fundamental explanations for aeronautical engineeringstudents and practicing engineers • Features a solutions manual to sample questions on the book’scompanion website Companion website - ahref="http://www.wiley.com/go/sadraey"www.wiley.com/go/sadraey/a

Advanced Aircraft Design

Author: Egbert Torenbeek
Publisher: John Wiley & Sons
ISBN: 1118568095
Size: 28.20 MB
Format: PDF
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Although the overall appearance of modern airliners has notchanged a lot since the introduction of jetliners in the 1950s,their safety, efficiency and environmental friendliness haveimproved considerably. Main contributors to this have been gasturbine engine technology, advanced materials, computationalaerodynamics, advanced structural analysis and on-board systems.Since aircraft design became a highly multidisciplinary activity,the development of multidisciplinary optimization (MDO) has becomea popular new discipline. Despite this, the application of MDOduring the conceptual design phase is not yet widespread. Advanced Aircraft Design: Conceptual Design, Analysis andOptimization of Subsonic Civil Airplanes presents aquasi-analytical optimization approach based on a concise set ofsizing equations. Objectives are aerodynamic efficiency, missionfuel, empty weight and maximum takeoff weight. Independent designvariables studied include design cruise altitude, wing area andspan and thrust or power loading. Principal features ofintegrated concepts such as the blended wing and body and highlynon-planar wings are also covered. The quasi-analytical approach enables designers to compare theresults of high-fidelity MDO optimization with lower-fidelitymethods which need far less computational effort. Another advantageto this approach is that it can provide answers to “whatif” questions rapidly and with little computational cost. Key features: Presents a new fundamental vision on conceptual airplane designoptimization Provides an overview of advanced technologies for propulsionand reducing aerodynamic drag Offers insight into the derivation of design sensitivityinformation Emphasizes design based on first principles Considers pros and cons of innovative configurations Reconsiders optimum cruise performance at transonic Machnumbers Advanced Aircraft Design: Conceptual Design, Analysis andOptimization of Subsonic Civil Airplanes advances understandingof the initial optimization of civil airplanes and is a must-havereference for aerospace engineering students, applied researchers,aircraft design engineers and analysts.

Design And Analysis Of Composite Structures

Author: Christos Kassapoglou
Publisher: John Wiley & Sons
ISBN: 1118536940
Size: 33.75 MB
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New edition updated with additional exercises and two newchapters. Design and Analysis of Composite Structures: WithApplications to Aerospace Structures, 2nd Edition builds onthe first edition and includes two new chapters on compositefittings and the design of a composite panel, as well additionalexercises. The book enables graduate students andengineers to generate meaningful and robust designs of complexcomposite structures. A compilation of analysis and design methodsfor structural components made of advanced composites, it beginswith simple parts such as skins and stiffeners and progressesthrough to applications such as entire components of fuselages andwings. It provides a link between theory and day-to-day designpractice, using theory to derive solutions that are applicable tospecific structures and structural details used in industry. Starting with the basic mathematical derivation followed bysimplifications used in real-world design,Design and Analysisof Composite Structures: With Applications to Aerospace Structures,2nd Edition presents the level of accuracy and range ofapplicability of each method along with design guidelines derivedfrom experience combined with analysis. The author solves indetail examples taken from actual applications to show how theconcepts can be applied, solving the same design problem withdifferent methods based on different drivers (e.g. cost or weight)to show how the final configuration changes as the requirements andapproach change. Each chapter is followed by exercises thatrepresent specific design problems often encountered in theaerospace industry but which are also applicable in the in theautomotive, marine, and construction industries. Updated to include additional exercises, that represent realdesign problems encountered in the aerospace industry, but whichare also applicable in the in the automotive, marine, andconstruction industries. Includes two new chapters. One on composite fittings andanother on application and the design of a composite panel. Provides a toolkit of analysis and design methods that enableengineers and graduate students to generate meaningful and robustdesigns of complex composite structures. Provides solutions that can be used in optimization schemeswithout having to run finite element models at each iteration; thusspeeding up the design process and allowing the examination of manymore alternatives than traditional approaches. Supported by a complete set of lecture slides and solutions tothe exercises hosted on a companion website for instructors. An invaluable resource for Engineers and graduate students inaerospace engineering as well as Graduate students and engineers inmechanical, civil and marine engineering.

Introduction To Aircraft Aeroelasticity And Loads

Author: Jan R. Wright
Publisher: John Wiley & Sons
ISBN: 1118700430
Size: 19.79 MB
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Introduction to Aircraft Aeroelasticity and Loads, SecondEdition is an updated new edition offering comprehensivecoverage of the main principles of aircraft aeroelasticity andloads. For ease of reference, the book is divided into three partsand begins by reviewing the underlying disciplines of vibrations,aerodynamics, loads and control, and then goes on to describesimplified models to illustrate aeroelastic behaviour and aircraftresponse and loads for the flexible aircraft before introducingsome more advanced methodologies. Finally, it explains howindustrial certification requirements for aeroelasticity and loadsmay be met and relates these to the earlier theoretical approachesused. Key features of this new edition include: Uses a unified simple aeroelastic model throughout thebook Major revisions to chapters on aeroelasticity Updates and reorganisation of chapters involving FiniteElements Some reorganisation of loads material Updates on certification requirements Accompanied by a website containing a solutions manual, andMATLAB® and SIMULINK® programs that relate to the modelsused For instructors who recommend this textbook, a series oflecture slides are also available Introduction to Aircraft Aeroelasticity and Loads, SecondEdition is a must-have reference for researchers andpractitioners working in the aeroelasticity and loads fields, andis also an excellent textbook for senior undergraduate and graduatestudents in aerospace engineering.

Theoretical And Computational Aerodynamics

Author: Tapan K. Sengupta
Publisher: John Wiley & Sons
ISBN: 1118787579
Size: 40.70 MB
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Aerodynamics has seen many developments due to the growth of scientific computing, which has caused the design cycle time of aerospace vehicles to be heavily reduced. Today computational aerodynamics appears in the preliminary step of a new design, relegating costly, time-consuming wind tunnel testing to the final stages of design. Theoretical and Computational Aerodynamics is aimed to be a comprehensive textbook, covering classical aerodynamic theories and recent applications made possible by computational aerodynamics. It starts with a discussion on lift and drag from an overall dynamical approach, and after stating the governing Navier-Stokes equation, covers potential flows and panel method. Low aspect ratio and delta wings (including vortex breakdown) are also discussed in detail, and after introducing boundary layer theory, computational aerodynamics is covered for DNS and LES. Other topics covered are on flow transition to analyse NLF airfoils, bypass transition, streamwise and cross-flow instability over swept wings, viscous transonic flow over airfoils, low Reynolds number aerodynamics, high lift devices and flow control. Key features: Blends classical theories of incompressible aerodynamics to panel methods Covers lifting surface theories and low aspect ratio wing and wing-body aerodynamics Presents computational aerodynamics from first principles for incompressible and compressible flows Covers unsteady and low Reynolds number aerodynamics Includes an up-to-date account of DNS of airfoil aerodynamics including flow transition for NLF airfoils Contains chapter problems and illustrative examples Accompanied by a website hosting problems and a solution manual Theoretical and Computational Aerodynamics is an ideal textbook for undergraduate and graduate students, and is also aimed to be a useful resource book on aerodynamics for researchers and practitioners in the research labs and the industry.

Stability And Control Of Aircraft Systems

Author: Roy Langton
Publisher: John Wiley & Sons
ISBN: 9780470058497
Size: 33.56 MB
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In the current climate of increasing complexity and functional integration in all areas of engineering and technology, stability and control are becoming essential ingredients of engineering knowledge. Many of today’s products contain multiple engineering technologies, and what were once simple mechanical, hydraulic or pneumatic products now contain integrated electronics and sensors. Control theory reduces these widely varied technical components into their important dynamic characteristics, expressed as transfer functions, from which the subtleties of dynamic behaviours can be analyzed and understood. Stability and Control of Aircraft Systems is an easy-to-read and understand text that describes control theory using minimal mathematics. It focuses on simple rules, tools and methods for the analysis and testing of feedback control systems using real systems engineering design and development examples. Clarifies the design and development of feedback control systems Communicates the theory in an accessible manner that does not require the reader to have a strong mathematical background Illustrated throughout with figures and tables Stability and Control of Aircraft Systems provides both the seasoned engineer and the graduate with the know-how necessary to minimize problems with fielded systems in the area of operational performance.