Accession Number : AD0601805

Title :   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.

Corporate Author : GRUMMAN AIRCRAFT ENGINEERING CORP BETHPAGE N Y

Personal Author(s) : Kaufman,Louis G. ,II.

Report Date : MAY 1964

Pagination or Media Count : 159

Abstract : 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.

Descriptors :   (*AERODYNAMIC CONTROL SURFACES, HYPERSONIC FLOW), (*FLAT PLATE MODELS, AERODYNAMIC CHARACTERISTICS), TRAILING CONTROL SURFACES, AERODYNAMIC HEATING, COOLING, REYNOLDS NUMBER, ANGLE OF ATTACK, HYPERSONIC WIND TUNNELS, SURFACE TEMPERATURE, REENTRY VEHICLES, BOOST GLIDE VEHICLES

Distribution Statement : APPROVED FOR PUBLIC RELEASE