PRESSURE AND HEAT TRANSFER MEASUREMENTS FOR MACH 8 FLOWS OVER A BLUNT PYRAMIDAL CONFIGURATION WITH AERODYNAMIC CONTROLS. PART 3: HEAT TRANSFER DATA FOR DELTA WING SURFACE
GRUMMAN AIRCRAFT ENGINEERING CORP BETHPAGE NY
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The report presents heat transfer data obtained in the AEDC 50-inch Mach 8 tunnel on the lower surface of a blunt pyramidal configuration having remotely controlled trailing edge flaps.