Document Details


Title:
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
Author(s):
Burkland, C V [North American Aviation, Inc.]
Document Type:
REPORT
Publication Date:
1952 Apr 09
Document Pages:
98 p.
Document Number(s):
SC-2583(TR); ALSNL199700000763
Originating Research Org.:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
OpenNet Entry Date:
1999 Sep 28
Description/Abstract:
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.


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