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.

Author(s):

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2002

Pub. Year:

2002

No.:

2002-0575

Paper no.:

2002-0575

Pages:

7

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00001706
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	40th
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	2002.01.14-2002.01.17
Note for article:	40th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 14-17 January 2002

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