NASA-TM-X-311-1960
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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NASA-TM-X-311-1960
Standard No.
NASA-TM-X-311-1960
Release Date
1960
Published By
National Aeronautics and Space Administration (NASA)
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