Reynolds number effects on unsteady boundary layer for an oscillating airfoil

Reynolds number effects on unsteady boundary layer for an oscillating airfoil

Author(s):

Kim, Dong Ha ( Korea Aerospace University, Goyang-city, Gyeonggi-do, 412-791, Republic of Korea )
Chang, Jo Won

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Applied Aerodynamics Conference

Ser. no.:

2009

Pub. Year:

2009

No.:

2009-3501

Paper no.:

AIAA Paper 2009-3501

Pages:

13

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200907

Type:

Technical Paper

Details

TDL ID:	ZA00066597
Series ID:	PA00000157
Conf. info. (Name):	AIAA Applied Aerodynamics Conference
Conf. info. (Number):	27
Conf. info. (Venue):	San Antonio, Texas
Conf. info. (Date):	2009.06.22-2009.06.25
Note for article:	DOI:10.2514/6.2009-3501 // 27th AIAA Applied Aerodynamics Conference 22 - 25 June 2009, San Antonio, Texas

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