A flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap
Description:
Report presenting flight tests made with a modified Ryan ST airplane to determine the effect on aileron characteristics of various arrangements of balanced split flaps covering that portion of the wing span occupied by the ailerons. With the flaps fully extended, the aileron effectiveness was reduced by approximately 18 percent of the effectiveness measured with ailerons alone.
Date:
May 1942
Creator:
Williams, W. C.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department