Some recent research on airfoil dynamic stall tentatively defines the boundary-layer flow processes during dynamic stall and suggests an approach to airfoil design for stall delay. The effect of changes of airfoil leading-edge radius and camber on increments in maximum lift coefficients is estimated, using a simple criterion for leading-edge stall. (Author)
Some Recent Research on Airfoil Dynamic Stall with Application to Airfoil Design
1971
27 pages
Report
Keine Angabe
Englisch
Adaptive Airfoil Dynamic Stall Control
Online Contents | 2007
|Adaptive Airfoil Dynamic Stall Control
AIAA | 2005
|Adaptive Airfoil Dynamic Stall Control
British Library Conference Proceedings | 2005
|Adaptive Airfoil Dynamic Stall Control
AIAA | 2007
|NTRS | 1969
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