NASA-TM-X-311
A wind-tunnel investigation of the aerodynamic characteristics of bodies of revolution at mach numbers of 2.37, 2.98, and 3.90 at angles of attack to 90 deg
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Abstract:
High angle aerodynamic characteristics produced by nose cone of revolution in wind tunnel at supersonic speed
Author(s):
F.M. Smith
Indexed under:
- None
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