Numerical Simulation on Separation of Scaled Supersonic Experimental Airplane from Rocket Booster at Supersonic Speed.

Numerical Simulation on Separation of Scaled Supersonic Experimental Airplane from Rocket Booster at Supersonic Speed.

著者名:

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : AIAA Fluid Dynamics Conference

シリーズ巻号:

2002

発行年:

2002

通号:

2002-2843

ペーパー番号:

2002-2843

総ページ数:

9

出版情報:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

言語:

英語

請求記号:

A07400

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001702
シリーズID:	PA00000147
会議名:	AIAA Fluid Dynamics Conference and Exhibit
回次:	32nd
会議開催地:	St. Louis, MO
会議開催年:	2002.06.24-2002.06.26
論文注記:	32nd AIAA Fluid Dynamics Conference and Exhibit, St. Louis, Missouri, 24-26 June 2002

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