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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