A flight investigation of the practical problems associated with porous-leading-edge suction
Description:
From Summary: "A flight investigation has been made of the practical problems associated with the use of porous-leading-edge suction. The wing leading edge of the test airplane was porous over approximately 83 percent of the span and the first 8 percent of the chord on the upper surface. Various other extents of suction area within these limits were also tested."
Date:
February 1954
Creator:
Hunter, Paul A. & Johnson, Harold I.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department