Pressure Measurements for Mach 8 Flows Over Expansion Corners and Ramps on an Internally Cooled Model Part III. Flows Over Full Span Ramps Mounted on a Flat Plate

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Report Number: RTD TDR 63-4044 Part 3
Author(s): Kaufman, Louis G., II
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Pages: 158
Contract: AF 33(616)-8130
DoD Project: 8219
DoD Task: 821902
Identifier: AD0601805

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Provenance: Bombardier/Aero

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