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Influence of wind tunnel freestream turbulence level on boundary-layer separation

Influence of wind tunnel freestream turbulence level on boundary-layer separation Abstract An investigation of aerodynamic performance for micro air vehicle (MAV) wing is performed. It is shown, what is a reason of significant wing performance difference between tests, which were carried out in different wind tunnels. New method for estimation of wind tunnel condition influence on experimental results is suggested. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Thermophysics and Aeromechanics Springer Journals

Influence of wind tunnel freestream turbulence level on boundary-layer separation

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References (19)

Publisher
Springer Journals
Copyright
2011 Pleiades Publishing, Ltd.
ISSN
0869-8643
eISSN
1531-8699
DOI
10.1134/S0869864311020028
Publisher site
See Article on Publisher Site

Abstract

Abstract An investigation of aerodynamic performance for micro air vehicle (MAV) wing is performed. It is shown, what is a reason of significant wing performance difference between tests, which were carried out in different wind tunnels. New method for estimation of wind tunnel condition influence on experimental results is suggested.

Journal

Thermophysics and AeromechanicsSpringer Journals

Published: Jun 1, 2011

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