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, c2006
4th ed
大学図書館所蔵 全25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
注記
Includes bibliographical references (p. 817-823) and index
内容説明・目次
内容説明
Winner of the Summerfield Book Award, winner of the Aviation-Space Writers Association Award of Excellence, and with over 30,000 copies sold, this is consistently the top-selling AIAA textbook title. This highly regarded textbook presents the entire process of aircraft conceptual design - from requirements definition to initial sizing, configuration layout, analysis, sizing, and trade studies - in the same manner seen in industry aircraft design groups. Interesting and easy to read, the book has more than 900 pages of design methods, illustrations, tips, explanations, and equations, and has extensive appendices with key data essential to design. The book is the required design text at numerous universities around the world and is a favorite of practicing design engineers. The new fourth edition is enhanced in many areas, with improvements and reworking of the text, expanded sizing and analysis methods, and up-to-date treatments of emerging technologies and concepts. A new section provides an introduction to spaceflight and rockets including thrust analysis and vehicle sizing for launch and planetary missions. Appendices are revised and additional exam questions are provided.
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
- * Appendix A: Unit Conversion
- * Appendix B: Standard Atmosphere.
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