Heat Transfer and Boundary Layer Growth for Ultra High Reynolds Number Compresible Turbulent Boundary Layers for a Radiativery Driven Hypersonic Wind Tunnel.

Heat Transfer and Boundary Layer Growth for Ultra High Reynolds Number Compresible Turbulent Boundary Layers for a Radiativery Driven Hypersonic Wind Tunnel.

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:

2002

発行年:

2002

通号:

2002-0575

ペーパー番号:

2002-0575

総ページ数:

7

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:	ZA00001706
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	40th
会議開催地:	Reno, NV
会議開催年:	2002.01.14-2002.01.17
論文注記:	40th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 14-17 January 2002

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