Pressure Measurements For Mach 8 Flows Over Expansion Corners And Ramps On An Internally Cooled Model. Part I. Expansion Corner Flows. Part Of An Investigation Of Hypersonic Flow Separation And Control Characteristics
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Report Number: RTD TDR 63-4044 Part 1
Author(s): Kaufman, Louis G., II
Corporate Author(s): Grumman Aircraft Engineering Corp Bethpage N Y
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1963-10
Pages: 73
Contract: AF 33(616)-8130
DoD Project: 8219
DoD Task: 821902
Identifier: AD0431280
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: AFRL/VACA
Author(s): Kaufman, Louis G., II
Corporate Author(s): Grumman Aircraft Engineering Corp Bethpage N Y
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1963-10
Pages: 73
Contract: AF 33(616)-8130
DoD Project: 8219
DoD Task: 821902
Identifier: AD0431280
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: AFRL/VACA