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An Investigation of Separated Flow About a Hemisphere-Cylinder at 0- to 19-Deg Incidence in the Mach Number Range from 0.6 to 1.5
Author(s): Hsieh, T.
Corporate Author(s): ARO, Inc.
Laboratory: Propulsion and Wind Tunnel Facility
Date of Publication: 1976-11
Report number: AEDC TR 76-112
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An Aerodynamic Coefficient Prediction Technique for Slender Bodies with Low Aspect Ratio Fins at Mach Numbers from 0.6 to 3.0 and Angles of Attack from 0 to 180 Degrees
Author(s): Baker, William B., Jr.
Corporate Author(s): ARO, Inc.
Laboratory: Propulsion and Wind Tunnel Facility
Date of Publication: 1978-03
Report number: AEDC TR 77-97

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