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Flow Properties of an Unyawed 10-Deg Cone for Gamma = 1.28 to 1.40 at Mach Numbers of 1.5 to 8
Author(s): Strike, W. T., Jr., Norton, B. B., Jr.Corporate Author(s): VKF, ARO, Inc.
Date of Publication: 1960-10
Report number: AEDC TN 60-178
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Test Section Turbulence in the AEDC/VKF Supersonic/Hypersonic Wind Tunnels
Author(s): Strike, W. T., Jr., Donaldson, J. C., Beale, D. K.Corporate Author(s): Arnold Engineering Development Center
Date of Publication: 1981-07-01
Report number: AEDC TR 81-5
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