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Pressure and Heat Transfer Measurements at Mach 5 and 8 for a Fin-Flat Plate Model: Part of an Investigation of Hypersonice Flow Separation and Control Characteristics

Title: Pressure and Heat Transfer Measurements at Mach 5 and 8 for a Fin-Flat Plate Model: Part of an Investigation of Hypersonice Flow Separation and Control Characteristics
Date: 1963
Index Abstract: Limited
Photo Quality: Incomplete
Report Number: ASD TDR 63-235
Creator: Kaufman, Louis G.; Meckler, Lawrence
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Extent: 121
Identifier: AD0406724
Access Rights: NA
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: 1963-04
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: AFRL/VACA
Type: report