Document Details

Results of Force Tests of Doorknob Model in the Sandia Corporation 12-inch Transonic Wind Tunnel (Program III-20)
Arnold, J W [Organization 5142]
Document Type:
Publication Date:
1957 Oct 15
Document Pages:
62 p.
Document Number(s):
SC-TM-282-57(51); ALSNL199700001044
Originating Research Org.:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
OpenNet Entry Date:
1999 Sep 28
OpenNet Modified Date:
1999 Sep 28
Wind tunnel aerodynamic test results on Doorknob instrumentation missile for high altitude nuclear tests. Lift, drag, and pitching moment coefficients at nominal Mach Nos. of 0.7, 0.8, 0.9, 1.0, 1.1, 1.2, and 1.3.

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