The drag of airplane wheels, wheel fairings, and landing gears - 3
Description:
The tests reported in this report conclude the investigation of landing-gear drag that has been carried out in the NACA 20-foot wind tunnel. They supplement earlier tests (reported in Technical Report No. 485) made with full-scale dummy wheels, wheel fairings, and landing gears intended for airplanes of 3,000 pounds gross weight and include tests of tail wheels and tail skids.
Date:
November 21, 1934
Creator:
Herrnstein, William H., Jr. & Biermann, David
Item Type:
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