Wall-Pressure Measurements in a Mach 3 Shock-Wave Turbulent Boundary Layer Interaction at a DNS Accessible Reynolds Number

Wall-Pressure Measurements in a Mach 3 Shock-Wave Turbulent Boundary Layer Interaction at a DNS Accessible Reynolds Number

Author(s):

M. Ringuette ( Princeton University, Princeton, NJ )
A. Smits

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Fluid Dynamics Conference

Ser. no.:

2007

Pub. Year:

2007

No.:

2007-4113

Paper no.:

AIAA Paper 2007-4113

Pub. info.:

Reston, Va: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200714 [CD-ROM 2007 Disc 14]

Type:

Technical Paper

Details

TDL ID:	ZA00049504
Series ID:	PA00000147
Conf. info. (Name):	AIAA Fluid Dynamics Conference and Exhibit
Conf. info. (Number):	37th
Conf. info. (Venue):	Miami, Florida
Conf. info. (Date):	2007.06.25-2007.06.28
Note for article:	37th AIAA Fluid Dynamics Conference and Exhibit, Miami, Florida, June 25-28, 2007

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