Aircraft design : a conceptual approach
著者
書誌事項
Aircraft design : a conceptual approach
(AIAA education series)
American Institute of Aeronautics and Astronautics, 1999
3rd ed
大学図書館所蔵 全22件
  青森
  岩手
  宮城
  秋田
  山形
  福島
  茨城
  栃木
  群馬
  埼玉
  千葉
  東京
  神奈川
  新潟
  富山
  石川
  福井
  山梨
  長野
  岐阜
  静岡
  愛知
  三重
  滋賀
  京都
  大阪
  兵庫
  奈良
  和歌山
  鳥取
  島根
  岡山
  広島
  山口
  徳島
  香川
  愛媛
  高知
  福岡
  佐賀
  長崎
  熊本
  大分
  宮崎
  鹿児島
  沖縄
  韓国
  中国
  タイ
  イギリス
  ドイツ
  スイス
  フランス
  ベルギー
  オランダ
  スウェーデン
  ノルウェー
  アメリカ
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.
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