Pressure-Sensitive Paint Application to a Wing-Body Model in a Hypersonic Shock Tunnel.

Pressure-Sensitive Paint Application to a Wing-Body Model in a Hypersonic Shock Tunnel.

著者名:

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : AIAA Aerodynamic Measurement Technology and Ground Testing Conference

シリーズ巻号:

2002

発行年:

2002

通号:

2002-2911

ペーパー番号:

2002-2911

総ページ数:

14

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:	ZA00001701
シリーズID:	PA00000173
会議名:	AIAA Aerodynamic Measurement Technology and Ground Testing Conference
回次:	22nd
会議開催地:	St. Louis, MO
会議開催年:	2002.06.24-2002.06.26
論文注記:	22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, St. Louis, Missouri, 24-26 June 2002

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