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The drag of airplane wheels, wheel fairings, and landing gears 2: nonretractable and partly retractable landing gears
This is the second report giving the results obtained in the NACA 20-foot wind tunnel on the drag due to landing gears. The present report gives the results of tests of nonretractable and partly retractable landing gears intended for heavier low-wing monoplanes of the transport and bomber type.
Date:
June 21, 1934
Creator:
Biermann, David & Herrnstein, William H., Jr.
System:
The UNT Digital Library