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Pressure Distributions and Oil Film Photographs for Mach 5 Flows Past Fins Mounted on a Flat Plate: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics

Report Number: ASD TDR 63-755
Author(s): Louis G. Kaufman
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Pages: 38
Contract: AF 33(616)-8130
Project: 8219
Task: 821902
AD Number: AD0422031

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