Aeroelastic Dynamics of a NACA 0012 Airfoil in the Transitional Reynolds Number Regime

Aeroelastic Dynamics of a NACA 0012 Airfoil in the Transitional Reynolds Number Regime

Author(s):

Publication title:

Proceedings of the ASME Pressure Vessels and Piping Conference 2006. Volume 9. 6th symposium on fluid-structure interactions, aeroelasticity and flow-induced vibration and noise : presented at 2006 ASME Pressure Vessels and Piping Conference, July 23-27, 2006, Vancouver, BC, Canada

Title of ser.:

Proceedings of the ASME Pressure Vessels and Piping Division

Ser. no.:

2006(9)

Pub. Year:

2007

Vol.:

9

Paper no.:

PVP2006-ICPVT 11-93957

Page(from):

847

Page(to):

854

Pages:

8

Pub. info.:

New York: American Society of Mechanical Engineers

ISBN:

9780791847886 [0791847888]

Language:

English

Call no.:

A11715/2006

Type:

Conference Proceedings

Details

TDL ID:	ZA00047094
Series ID:	PA00000033
Conf. info. (Name):	ASME Pressure Vessels and Piping Conference ; Symposium on fluid-structure interactions, aeroelasticity and flow-induced vibration and noise
Conf. info. (Number):	2006 ; 6th
Conf. info. (Venue):	Vancouver, BC, Canada
Conf. info. (Date):	2006.07.23-2006.07.27

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