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E-raamat: Introduction to Aircraft Design

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(Cranfield University, UK)
  • Formaat: PDF+DRM
  • Sari: Cambridge Aerospace Series
  • Ilmumisaeg: 03-Apr-2017
  • Kirjastus: Cambridge University Press
  • Keel: eng
  • ISBN-13: 9781108110846
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Introduction to Aircraft DesignSuurem pilt
  • Formaat: PDF+DRM
  • Sari: Cambridge Aerospace Series
  • Ilmumisaeg: 03-Apr-2017
  • Kirjastus: Cambridge University Press
  • Keel: eng
  • ISBN-13: 9781108110846
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The new edition of this popular textbook provides a modern, accessible introduction to the whole process of aircraft design from requirements to conceptual design, manufacture and in-service issues. Highly illustrated descriptions of the full spectrum of aircraft types, their aerodynamics, structures and systems, allow students to appreciate good and poor design and understand how to improve their own designs. Cost data is considerably updated, many new images have been added and new sections are included on the emerging fields of Uninhabited Aerial Vehicles and environmentally-friendly airlines. Examples from real aircraft projects are presented throughout, demonstrating to students the applications of the theory. Three appendices and a bibliography provide a wealth of information, much not published elsewhere, including simple aerodynamic formulae, an introduction to airworthiness and environmental requirements, aircraft, engine and equipment data, and a case study of the conceptual design of a large airliner.

The new edition of this popular textbook provides a modern, accessible introduction to the whole process of aircraft design from requirements to conceptual design, manufacture and in-service issues. The text includes updated costs, many new images and examples from real projects and unique data that's invaluable to aircraft designers' work.

Muu info

This new edition provides a modern, accessible introduction to the whole process of aircraft design together with invaluable data.
Preface xiii
Acknowledgements xv
1 Introduction
1(5)
1.1 Why Another Aircraft Design Book?
1(1)
1.2 Topics
1(1)
1.3 The Design Process
2(4)
2 Why Should We Design a New Aircraft?
6(14)
2.1 Market Surveys
6(2)
2.2 Operator-Derived Specifications
8(3)
2.3 Specification for a Close Air Support Aircraft
11(2)
2.4 Requirements for an Uninhabited Combat Air Vehicle
13(1)
2.5 Airline Specifications for a 150-seat Airliner
14(6)
3 Why is it That Shape?: Civil Aircraft
20(20)
3.1 Background
20(6)
3.2 Civil Aircraft Types
26(14)
4 Why is it That Shape?: Other Types
40(25)
4.1 Military Aircraft Types
40(14)
4.2 Rotorcraft, V/STOL Aircraft and Uninhabited Aerial Systems
54(11)
5 What's Under the Skin?: Structure and Propulsion
65(18)
5.1 General
65(1)
5.2 The Structure
65(8)
5.3 Propulsion: the Primary Power System
73(10)
6 What's Under the Skin?: Airframe Systems
83(18)
6.1 Secondary Power Systems
83(6)
6.2 The Fuel System
89(4)
6.3 Furnishings
93(1)
6.4 Safety Installations
93(1)
6.5 Landing Gear Installations
94(5)
6.6 Recent Innovations in Airframe Systems
99(2)
7 What's under the skin?: Avionics, Flight Control and Weapon Systems
101(21)
7.1 Avionic Systems
101(8)
7.2 Flight Control Systems
109(4)
7.3 Weapon Systems
113(9)
8 Why do Aircraft Cost so Much?
122(22)
8.1 General
122(1)
8.2 Acquisition Costs (The Costs of Buying or Acquiring the Aircraft)
122(5)
8.3 Civil Aircraft Operating Costs
127(1)
8.4 Military Aircraft Life-Cycle Costs
128(2)
8.5 The Costs of Reliability and Maintainability
130(14)
9 What Help Can I Get?: Bibliography and Computer-Aided Design
144(21)
9.1 Aircraft Design Bibliography
144(3)
9.2 Data Sheets, Airworthiness Requirements and Environmental Targets
147(4)
9.3 Computer Design Tools
151(5)
9.4 The Integration of Computer Tools as Part of Concurrent Engineering
156(1)
9.5 Classic Computer-Aided Design Systems
157(8)
10 The Shape of Things to Come: Should the Project Continue?
165(15)
10.1 Introduction
165(1)
10.2 Conceptual Design Definition
165(1)
10.3 Comparison and Choice
166(1)
10.4 Simple Decision-Making Techniques
166(1)
10.5 Example of a Conceptual Aircraft Design Definition Description: The Cranfield A-90
167(10)
10.6 Progress of the A-90 Project beyond the Conceptual Design Stage
177(3)
11 What Can Go Wrong?: Some Lessons from Past Aircraft Projects, and a Glimpse into the Future
180(22)
11.1 Introduction
180(1)
11.2 Aircraft that Suffered from Requirements that were too Restrictive, too Ambitious or were Changed during Development
180(5)
11.3 Projects that were Overtaken by Events
185(3)
11.4 A Step Too Far or Too Soon?
188(3)
11.5 Some Challenging Future Projects
191(8)
11.6 Conclusions
199(3)
Appendix A Useful Aircraft Design Data
202(64)
A1 Introduction
202(1)
A2 US/UK Nomenclature
202(1)
A3 UK and US/SI Conversion Tables and Airspeed Charts
203(3)
A4 Aircraft Leading Data Tables
206(13)
A5 Powerplant Data
219(17)
A6 Aerodynamic Data
236(8)
A7 Structures and Materials Data
244(2)
A8 Landing-Gear Data
246(1)
A9 Aircraft Interior Data
247(13)
A10 Aircraft Weapons
260(6)
Appendix B A-90 Parametric Study. Example: The A-90 500-Seat Airliner
266(11)
B1 Introduction
266(1)
B2 Landing Field Distance
266(2)
B3 Take-Off Field Length
268(1)
B4 Second Segment Climb
269(1)
B5 Missed Approach
270(1)
B6 Cruise Performance
271(2)
B7 Ceiling with One Engine Inoperative
273(2)
B8 Arrival at the Match Point
275(2)
Appendix C The Prediction of Aircraft Reliability and Maintainability Targets
277(5)
C1 Introduction
277(1)
C2 Commercial Aircraft Dispatch Reliability Prediction
277(5)
References 282(5)
Index 287
John Fielding is Professor Emeritus and the former Head of the Aerospace Engineering Group in the School of Engineering, Cranfield University, UK. His research, teaching and continuing consulting focused on aircraft design, reliability, maintainability and operational effectiveness.
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