Increment of lift due to sharp edged gust that moves across 2-dimensional airfoil at relative velocity different from flight velocity, is calculated on assumption of incompressible flow; application of results to helicopter blade wing interference.
Aerodynamic force on airfoil in moving gust
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 23 , n 11
1956
7 pages
Aufsatz (Zeitschrift)
Englisch
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