Title:
Results of Wind-Tunnel Tests of the Second Series of Aerodynamic Shapes Proposed For Use As a Short-7 Weapon
Publication Date:
1957 Jun 25
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
Description/Abstract:
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.