Pressure Measurements For Mach 8 Flows Over Expansion Corners And Ramps On An Internally Cooled Model. Part II. Flows Over A Flat Plate With And Without A Partial Span Ramp.
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Report Number: RTD TDR 63-4044 Part 2
Author(s): Kaufman, Louis G., II
Corporate Author(s): Grumman Aircraft Engineering Corp Bethpage N Y
Date of Publication: 1964-10
Pages: 184
DoD Task:
Identifier: AD0609458
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control
Author(s): Kaufman, Louis G., II
Corporate Author(s): Grumman Aircraft Engineering Corp Bethpage N Y
Date of Publication: 1964-10
Pages: 184
DoD Task:
Identifier: AD0609458
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control