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Pressure and Heat Transfer Measurements fro Mach 21 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls

Title: Pressure and Heat Transfer Measurements fro Mach 21 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls
Date: 1964
Index Abstract: Coming Soon
Photo Quality: Complete
Report Number: FDL TDR 64-120
Corporate Author: Grumman Aircraft Engineering Corporation
Extent: 50
Identifier: AD0609559
Access Rights: OTS
Distribution Classification: 1
Contract: AF 33(616)-8130
DoD Project: 8219
DoD Task: 821902
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Abstract: Pressure and heat transfer data were obtained for Mach 21 flows over a blunt pyramidal configuration composed of a 70 degree sweepback delta wing surface and two dihedral surfaces. Instrumented trailing edge flaps were mounted in pairs on either the delta wing or dihedral surfaces and an uninstrumented ventral fin was attached during several test runs. The model was pitched at angles of attack between -30 and +45 degrees for free stream Reynolds numbers, based on model length, of approximately 51,000.
Report Availability: Full text available
Date Issued: 1964-08
Laboratory: AF Flight Dynamics Laboratory
Provenance: Lockheed Martin Missiles & Fire Control; AFRL/VACA
Type: report
Format: 1 online resource
Creator: Kaufman, Louis G., II