Global Heat Transfer Measurement in a Hypersonic Shock Tunnel using Temperature-Sensitive Paint.

Global Heat Transfer Measurement in a Hypersonic Shock Tunnel using Temperature-Sensitive Paint.

著者名:

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

2003

発行年:

2003

通号:

2003-0743

ペーパー番号:

2003-0743

総ページ数:

12

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:	ZA00001712
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	41st
会議開催地:	Reno, NV
会議開催年:	2003.01.06-2003.01.09
論文注記:	41st AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 6-9 January 2003

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