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.
GRUMMAN AIRCRAFT ENGINEERING CORP BETHPAGE N Y
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The report presents data obtained on the upper, flat plate, surface of the model and on the face of a 25 chord, full span, ramp mounted on the trailing edge of the flat plate. Data were obtained for three ramp angles, both with and without internal cooling of the flat plate surface, for model angles of attack from -43 to 10 degrees for free stream Reynolds numbers per foot of 1.1, 2.2 and 3.3 million.