Effect of Chordwise Vanes on Amplitude of Tail Buffeting
Description:
"Flight tests have been made with a P-51D airplane to determine the effect of chordwise vanes on the amplitude of tail buffeting. The tests made during abrupt pull-ups to the buffeting boundary included strain measurements on wing and tail and tuft studies over the wing. The results indicate that the vanes tested have no appreciable effect on the amplitude of tail buffeting" (p. 1).
Date:
November 10, 1947
Creator:
Stokke, Allen R.
Item Type:
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