Document Details

Results of Wind-Tunnel Tests of the Second Series of Aerodynamic Shapes Proposed For Use As a Short-7 Weapon
Millwright, S S [Organization 5142]; Black, R L [Organization 5142]
Document Type:
Publication Date:
1957 Jun 25
Document Pages:
46 p.
Document Number(s):
SC-TM-168-57(51); ALSNL199700000565
Originating Research Org.:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
OpenNet Entry Date:
1999 Sep 28
OpenNet Modified Date:
1999 Sep 28
Stability coefficients obtained from tests conducted at the Sandia Corporation 3-inch open-jet wind tunnel are presented and compared with stability coefficients obtained from tests conducted at 3 larger wind tunnels-- a satisfactory aerodynamic shape.

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