Results of tests described applied to case of oscillating airfoil and problem of plane airfoil entering sharp edged gust; in latter case rate of increase of lift after entrance of airfoil into gust boundary is determined, it is shown that during entire process lift acts at quarter chord point of airfoil. Before Inst Aeronautical Sciences.
Airfoil theory for non-uniform motion
J Aeronautical Sciences
Journal of Aeronautical Sciences ; 5 , n 10
1938
12 pages
Bibliography
Article (Journal)
English
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Airfoil theory for non-uniform motion
Engineering Index Backfile | 1938
|On theory of unsteady motion of airfoil
Engineering Index Backfile | 1947
|On the Theory of the Unsteady Motion of an Airfoil
NTRS | 1947
|On the theory of the unsteady motion of an airfoil
TIBKAT | 1947
|AIAA | 1988
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