Aircraft engine design
著者
書誌事項
Aircraft engine design
(AIAA education series)
American Institute of Aeronautics and Astronautics, c2002
2nd ed
大学図書館所蔵 全10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 and index
内容説明・目次
内容説明
This text presents a complete and realistic aircraft engine design experience. From the request for proposal for a new aircraft to the final engine layout, the book provides the concepts and procedures required for the entire process. It is an expanded and updated version of the first edition that emphasizes contemporary developments impacting engine design such as theta break/throttle ratio, life management, controls, and stealth. The key steps of the process are detailed in ten chapters that encompass aircraft constraint analysis, aircraft mission analysis, engine parametric (design point) analysis, engine performance (off-design) analysis, engine installation drag and sizing, and the design of inlets, fans, compressors, main combustors, turbines, afterburners, and exhaust nozzles. The AEDsys software that accompanies the text provides comprehensive computational support for every design step. The software has been carefully integrated with the text to enhance both the learning process and productivity, and allows effortless transfer between British Engineering and SI units. The AEDsys software is furnished on CD and runs in the Windows operating system on PC-compatible systems.A user's manual is provided with the software, along with the complete data files used for the Air-to-Air Fighter and Global Range Airlifter design examples of the book.
目次
* The Design Process * Aircraft/Engine System Constraint Analysis * Mission Analysis * Engine Selection: Parametric Cycle Analysis * Engine Selection: Performance Cycle Analysis * Sizing the Engine: Installed Performance * Engine Component Design: Global and Interface Quantities * Engine Component Design: Rotating Turbomachinery * Engine Component Design: Combustion Systems * Engine Component Design: Inlets and Exhaust Nozzles * Appendix A: Units & Conversions * Appendix B: Altitude Tables * Appendix C: Engine Data * Appendix D: Engine Performance: Theta Break and Throttle Ratio * Appendix E: Aircraft Engine Thrust Measures * Appendix F: Compressible Flow Functions - Variable Specific Heats * Appendix G: Constant Area Mixer Analysis * Appendix H: Mixed Flow Turbofan Engine - Parametric Analysis Equations * Appendix I: Mixed Flow Turbofan Engine - Performance Analysis Equations * Appendix J: High Bypass Ratio Turbofan Engine * Appendix K: Turboprop Engine * Appendix L: Propeller Design Tools * Appendix M: Material Properties * Appendix N: Turbine Engine Life Management * Appendix O: Engine Controls * Appendix P: Global Range Airlifter (GRA) RFP * The Design Process * Aircraft/Engine System Constraint
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