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

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

Title: Pressure Measurement at Mach 19 for a Winged Re-Entry Configuration: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Date: 1963
Index Abstract: Limited
Photo Quality: Incomplete
Report Number: ASD TDR 63-319
Creator: Hartofilis, Stavros A.
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Division
Extent: 48
Identifier: AD0411127
Access Rights: ASTIA
Distribution Classification: 2
Contract: AF 33(616)-8130
DoD Project: 8219
DoD Task: 821902
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Report Availability: Not available via Contrails
Date Issued: 1963-05
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: AFRL/VACA
Type: report