Experimental Study of Tip Vortex Flow from a Periodically Pitched Airfoil Section (AIAA 2016-1846)
Aerospace sciences meeting
2016-01-01
19 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Vortex-Lift Mechanism in Axial Turbomachinery with Periodically Pitched Stators
Online Contents | 2016
|Airfoil-Gust Interactions in Transonic Flow (AIAA 2016-2872)
British Library Conference Proceedings | 2016
|Unsteady Aerodynamics and Trailing-edge Vortex Sheet of An Airfoil (AIAA 2016-1078)
British Library Conference Proceedings | 2016
|