Detection of boundary-layer transition in a cryogenic wind tunnel by using luminescent paint

Detection of boundary-layer transition in a cryogenic wind tunnel by using luminescent paint

Author(s):

Asai, K. ( National Aerospace Laboratory, Japan )
Kanda, H.
Kunimasu, T.
Liu, T.
Sullivan, J.P.

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : AIAA Advanced Measurement and Ground Testing Technology Conference

Ser. no.:

1996

Pub. Year:

1996

No.:

96-2185

Paper no.:

96-2185

Page(from):

1

Page(to):

11

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050834
Series ID:	PA00000145
Conf. info. (Name):	AIAA Advanced Measurement and Ground Testing Technology Conference
Conf. info. (Number):	19th
Conf. info. (Venue):	New Orleans, LA
Conf. info. (Date):	1996.06.17-1996.06.20
Note for article:	19th AIAA Advanced Measurement and Ground Testing Technology Conference, June 17-20, 1996/New Orleans, LA

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