Numerical Study on Effect of a Thermal Bump in Supersonic Flow Control

Numerical Study on Effect of a Thermal Bump in Supersonic Flow Control

Author(s):

H. Yan ( Wright State University, Dayton, OH )
D. Gaitonde ( U.S. Air Force Research Laboratory, Dayton, OH )

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Plasmadynamics and Lasers Conference

Ser. no.:

2008

Pub. Year:

2008

No.:

2008-3790

Paper no.:

AIAA Paper 2008-3790

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200807 [CD-ROM 2008 Disc 7]

Type:

Technical Paper

Details

TDL ID:	ZA00050894
Series ID:	PA00000148
Conf. info. (Name):	Plasmadynamics and Lasers Conference
Conf. info. (Number):	39th
Conf. info. (Venue):	Seattle, WA
Conf. info. (Date):	2008.06.23-2008.06.26
Note for article:	39th Plasmadynamics and Lasers Conference, 23-26 June 2008, Seattle, Washington

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