Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part III: Heat Transfer Data for Delta Wing Surface

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Report Number: FDL TDR 64-2 Part 3
Author(s): Kaufman, Louis G., II
Corporate Author(s): Grumman Aircraft Engineerign Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-05
Pages: 128
Contract: AF 33(616)-8130
DoD Project: 8219
DoD Task: 821902
Identifier: AD0601804

Abstract:
The report presents heat transfer data obtained in the AEDC 50-inch Mach 8 tunnel on the lower surface of a blunt pyramidal configuration having remotely controlled trailing edge flaps.

Provenance: AFRL/VACA

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