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Pressure Measurement at Mach 19 for a Winged Re-Entry Configuration: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics

Report Number: ASD TDR 63-319
Author(s): Stavros A. Hartofilis
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Division
Date of Publication: 1963-05
Pages: 48
Contract: AF 33(616)-8130
Project: 8219
Task: 821902
AD Number: AD0411127

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