A Numerical Study of Nozzle Boundary Layer Thickness on Axisymmetric Supersonic Jet Screech Tones

A Numerical Study of Nozzle Boundary Layer Thickness on Axisymmetric Supersonic Jet Screech Tones

Author(s):

J. Gao ( Beijing University of Aeronautics and Astronautics, Beijing, China (prc) )
X. Li

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA/CEAS Aeroacoustics Conference

Ser. no.:

2006

Pub. Year:

2006

No.:

2006-2675

Paper no.:

AIAA Paper 2006-2675

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200608 [CD-ROM 2006 Disc 8]

Type:

Technical Paper

Details

TDL ID:	ZA00047229
Series ID:	PA00000149
Conf. info. (Name):	AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference)
Conf. info. (Number):	12th
Conf. info. (Venue):	Cambridge, Massachusetts
Conf. info. (Date):	2006.05.08-2006.05.10

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