Aircraft design : a conceptual approach

著者

• Raymer, Daniel P.

書誌事項

Aircraft design : a conceptual approach

Daniel P. Raymer

（AIAA education series）

American Institute of Aeronautics and Astronautics, 1999

3rd ed

内容説明・目次

内容説明

This textbook presents the entire process of aircraft conceptual design - from requirements definition through initial sizing, congfiguration layout, analysis, sizing and trade studies - in the same manner seen in industry aircraft design groups. Interesting and easy to read, it contains more than 900 pages of design methods, illustrations, tips, explanations and equations, and has extensive appendices with key data essential to design. For the third edition, Daniel Raymer has updated his book to reflect advances in technologies such as hypersonics, stealth and STOVL, and design methods including concurrent engineering, cost as an independent variable, and the impact of the factory of the future. With his usual easy-to-read style, he has expanded his treatments of such key areas as jet engine installation, CFD, trim analysis, CAD/CAM, propeller thrust analysis, weights estimation, cost analysis and multivariable optimization.Raymer has added, by popular demand, a step-by-step description of how a typical design is developed (with illustrations), and also describes the technical concepts behind some unusual design approaches such as tailless, canard-pusher, no-lateral-symmetry (Rutan Boomerang), wing-in-ground effect, and the hypersonic waverider. Along with the addition of metric data and equations, more than 30 new illustrations and homework examples have been added.

目次

• Design - a separate discipline
• overview of the design process
• sizing from a conceptual sketch
• airfoil and geometry selection thrust-to-weight ratio and wing loading
• initial sizing
• configuration layout and loft
• special considerations in configuration layout
• crew station, passengers and payload
• propulsion and fuel system integration
• landing gear and subsystems
• intermission - step-by-step development of a new design
• aerodynamics
• propulsion
• structures and loads
• weights
• stability
• control and handling qualities
• performance and flight mechanics
• cost analysis
• sizing and trade studies
• design of unique aircraft concepts
• conceptual design examples. Appendices: unit conversion
• standard atmosphere, compressible flow and shocks
• airspeed
• airfoil data
• typical engine performance curves
• design requirements and specifications.

「Nielsen BookData」 より

詳細情報

• NII書誌ID(NCID): BA43281470
• ISBN:
  • 1563472813
• LCCN: 99029325
• 出版国コード: us
• タイトル言語コード: eng
• 本文言語コード: eng
• 出版地: Washington, D.C.
• ページ数/冊数: xviii, 923 p.
• 大きさ: 24 cm
• 分類:
  • LCC : TL671.2
  • DC21 : 629.134/1
• 件名:
  • LCSH : Airplanes -- Design and construction
• 親書誌ID:
  • BA04361955