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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
Model Study of Plans for Channel Improvement at Dogtooth Bend, Mississippi River, Folder 1
This memorandum, constitutes a report on the results of experiments conducted at the U. S. Waterways Experiment Station on a small scale model of that reach of the Mississippi River near and including Dogtooth Bend (Mile 32.7 above to Mile 4.0 below Cairo).
Date:
April 2, 1938
Creator:
Waterways Experiment Station (U.S.)
System:
The UNT Digital Library