Multidisciplinary Design Optimization of Supersonic Fughter Wing Using Response Surface Methodology

Multidisciplinary Design Optimization of Supersonic Fughter Wing Using Response Surface Methodology

著者名:

掲載資料名:

A collection of technical papers : 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Atlanta, Georgia, 4-6 September 2002

シリーズ名:

AIAA Paper : Symposium on Multidisciplinary Analysis and Optimization

シリーズ巻号:

2002

発行年:

2002

巻:

v. 1

通号:

2002-5408

ペーパー番号:

AIAA-2002-5408

開始ページ:

83

終了ページ:

92

総ページ数:

10

出版情報:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563475504 [1563475502]

言語:

英語

請求記号:

A07400/025400 (v.1)

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001458
シリーズID:	PA00000159
会議名:	AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
回次:	9th
会議開催地:	Atlanta, Georgia
会議開催年:	2002.09.04-2002.09.06

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