Simulation of Spinning Missile Flow Fields Using U2NCLE

Simulation of Spinning Missile Flow Fields Using U2NCLE

著者名:

掲載資料名:

A collection of technical papers : 20th AIAA Applied Aerodynamics Conference, St. Louis, Missouri, 24-27 June 2002

シリーズ名:

AIAA Paper : AIAA Applied Aerodynamics Conference

シリーズ巻号:

2002

発行年:

2002

通号:

2002-2797

ペーパー番号:

AIAA-2002-2797

開始ページ:

122

終了ページ:

132

総ページ数:

11

出版情報:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563475450 [1563475456]

言語:

英語

請求記号:

A07400/022712

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001451
シリーズID:	PA00000157
会議名:	AIAA Applied Aerodynamics Conference
回次:	20th
会議開催地:	St. Louis, Missouri
会議開催年:	2002.06.24-2002.06.27

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