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Flight Performance of Fixed and Rotary Wing Aircraft(2006) 요약정보 및 구매

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지은이 Filippone
발행년도 2006-05-10
페이지 565
ISBN 9780750668170
도서상태 구매가능
판매가격 40,000원
포인트 0점
배송비결제 주문시 결제

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  • Calculation and optimisation of flight performance is required to design or select new aircraft, efficiently operate existing aircraft, and upgrade aircraft. It provides critical data for aircraft certification, accident investigation, fleet management, flight regulations and safety. This book presents an unrivalled range of advanced flight performance models for both transport and military aircraft, including the unconventional ends of the envelopes. Topics covered include the numerical solution of supersonic acceleration, transient roll, optimal climb of propeller aircraft, propeller performance, long-range flight with en-route stop, fuel planning, zero-gravity flight in the atmosphere, VSTOL operations, ski jump from aircraft carrier, optimal flight paths at subsonic and supersonic speed, range-payload analysis of fixed- and rotary wing aircraft, performance of tandem helicopters, lower-bound noise estimation, sonic boom, and more.This book will be a valuable text for undergraduate and post-graduate level students of aerospace engineering. It will also be an essential reference and resource for practicing aircraft engineers, aircraft operations managers and organizations handling air traffic control, flight and flying regulations, standards, safety, environment, and the complex financial aspects of flying aircraft. This book: provides a unique coverage of fixed and rotary wing aircraft in a unified manner, including optimisation, emissions control and regulation; is ideal for students, aeronautical engineering capstone projects, and for widespread professional reference in the aerospace industry; gives comprehensive coverage of computer-based solution of aerospace engineering problems; the critical analysis of performance data; and case studies from real world engineering experience. It is supported by end of chapter exercises, an extensive Instructor's Manual and downloadable flight performance modelling code. 
  • Part 1. Fixed-Wing aircraft performance 1. Introduction 2. The aircraft and its environment 3. Weight performance 4. Aerodynamic performance 5. Engine performance 6. Flight envelopes 7. Take-off and landing 8. Climb and gliding 9. Cruise performance 10. Maneuver performance Part 2. Rotary- Wing Aircraft Performance 11. Rotorcraft performance 12. Rotorcraft in vertical flight 13. Rotorcraft in forward flight 14. Rotorcraft maneuver 15. Rotorcraft mission analysis Part 3. V/STOL and Noise Performance 16. V/STOL performance 17. Noise performance Appendix A Aircraft models Appendix B Noise data Appendix C Selected simulation programs Bibiography Index
  • Dr. Antonio Filippone is a faculty member in the Department of Mechanical, Aerospace and Civil Engineering at the University of Manchester, United Kingdom.
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