Supercritical Flow over Unstalled Plunging Airfoil Computed by Euler Method

Supercritical Flow over Unstalled Plunging Airfoil Computed by Euler Method

Author(s):

S. Yang ( University of California, Irvine, Irvine, CA )
S. Luo
F. Liu
H. Tsai ( National University of Singapore, Crescent, Singapore )

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2006

Pub. Year:

2006

No.:

2006-0293

Paper no.:

AIAA Paper 2006-293

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200604 [CD-ROM 2006 Disc 4]

Type:

Technical Paper

Details

TDL ID:	ZA00047219
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	44th
Conf. info. (Venue):	Reno, Nevada
Conf. info. (Date):	2006.01.09-2009.01.12

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