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Pressure distribution over a symmetrical airfoil section with trailing edge flap
"Measurements were made to determine the distribution of pressure over one section of an R. A. F. 30 (symmetrical) airfoil with trailing edge flaps. In order to study the effect of scale measurements were made with air densities of approximately 1 and 20 atmospheres. Isometric diagrams of pressure distribution are given to show the effect of change in incidence, flap displacement, and scale upon the distribution. Plots of normal force coefficient versus angle of attack for different flap displacements are given to show the effect of a displaced flap" (p. 589).
Date:
April 2, 1930
Creator:
Jacobs, Eastman N. & Pinkerton, Robert M.
System:
The UNT Digital Library