Low Speed Wind Tunnel Tests of the 0.2 Scale Model of the F-86D Airplane to Determine the Effect of the Asymmetrical Mounted External Stores TX-10 and TX-12
1952 Apr 09
Originating Research Org.:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
OpenNet Entry Date:
1999 Sep 28
This report presents data obtained from tests conducted in the North American Aerodynamics Lab. The test vehicle duplicated exactly the wing geometry of the F-86A, E, F, and H series airplanes. The tests were done from 12/20/51 to 1/4/52.