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Pressure and Heat Transfer Measurements at Mach 13 and 19 for Flows Ahead of Ramps, Over Expansion Corners, and Past Fin-Plate Combinations: Part of an Investigation of Hypersonic Flow Separation and Control CharacteristicsAuthor(s): Hatofilis, Stavros A.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-144