High performance supersonic missile inlet design using automated optimization

High performance supersonic missile inlet design using automated optimization

著者名:

Zha, Ge-Cheng ( Rutgers University - The State University of New Jersey )

掲載資料名:

6th AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization : a collection of technical papers, September 4-6, 1996, Bellevue, WA

シリーズ名:

AIAA Paper : Symposium on Multidisciplinary Analysis and Optimization

シリーズ巻号:

CP9611

発行年:

1996

巻:

pt. 2

通号:

96-4142

ペーパー番号:

AIAA 96-4142

開始ページ:

1355

終了ページ:

1371

出版情報:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563472183 [156347218X]

言語:

英語

請求記号:

(pt.1)A07400/963378,(pt.2)A07400/963379

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00007855
シリーズID:	PA00000159
会議名:	AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
回次:	6th
会議開催地:	Bellevue, WA
会議開催年:	1996.09.04-1996.09.06

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