A new shock tunnel facility for high compressibility mixing layer studies

A new shock tunnel facility for high compressibility mixing layer studies

Author(s):

Rossmann, Tobias ( High Temperature Gasdynamics Laboratory, Stanford University )
Mungal, M. Godfrey ( High Temperature Gasdynamics Laboratory, Stanford University )
Hanson, Ronald K. ( High Temperature Gasdynamics Laboratory, Stanford University )

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

1999

Pub. Year:

1999

No.:

99-0415

Paper no.:

99-0415

Page(from):

1

Page(to):

8

Pages:

8

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050873
Series ID:	PA00000138
Conf. info. (Name):	Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	37th
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	1999.01.11-1999.01.14
Note for article:	37th AIAA Aerospace Sciences Meeting, January 11-14, 1999/Reno, NV

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