Pressure and Heat Transfer Measurements fro Mach 21 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls
Item
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Title
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Pressure and Heat Transfer Measurements fro Mach 21 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls
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Date
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1964
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Index Abstract
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Coming Soon
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Photo Quality
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Complete
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Report Number
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FDL TDR 64-120
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Corporate Author
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Grumman Aircraft Engineering Corporation
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Extent
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50
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Identifier
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AD0609559
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Access Rights
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OTS
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Distribution Classification
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1
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Contract
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AF 33(616)-8130
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DoD Project
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8219
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DoD Task
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821902
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DTIC Record Exists
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No
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Distribution Change Authority Correspondence
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None
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Abstract
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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.
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Report Availability
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Full text available
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Date Issued
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1964-08
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Laboratory
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AF Flight Dynamics Laboratory
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Provenance
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Lockheed Martin Missiles & Fire Control
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AFRL/VACA
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Type
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report
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Format
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1 online resource
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Creator
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Kaufman, Louis G., II