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Aeroheating characteristics of the X-33 Rev-F configuration have been experimentally examined in the Langley 20-Inch Mach 6 Air Tunnel (Test 6770). Global surfa
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Aeroheating and boundary layer transition characteristics for the X-43 (Hyper-X) configuration have been experimentally examined in the Langley 31-Inch Mach 10
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Pages: 696
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Measurements have been made of the mean total-head and temperature fields in a round turbulent jet with various initial temperatures.