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

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

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Provenance: AFRL/VACA

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