Pressure-Distribution Measurements on the Tail Surfaces of a Rotating Model of the Design BFW - M31
Description:
In order to obtain insight into the flow conditions on tail surfaces on airplanes during spins, pressure-distribution measurements were performed on a rotating model of the design BFW-M31. For the time being, the tests were made for only one angle of attack (alpha = 60 degrees) and various angles of yaw and rudder angles. The results of these measurements are given; the construction of the model, and the test arrangement used are described. Measurements to be performed later and alterations pla…
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Date:
December 1949
Creator:
Kohler, M. & Mautz, W.
Item Type:
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