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.
The Drag of Airplane Wheels, Wheel Fairings, and Landing Gears - III
1936-01-01
Sonstige
Keine Angabe
Englisch
Drag of airplane wheels, wheel fairings, and landing gears
Engineering Index Backfile | 1934
|Engineering Index Backfile | 1935
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