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Heat-transfer measurements on a blunt spherical-segment nose to a Mach number of 15.1 and flight performance of the rocket-propelled model to a Mach number of 17.8

Title:Heat-transfer measurements on a blunt spherical-segment nose to a Mach number of 15.1 and flight performance of the rocket-propelled model to a Mach number of 17.8
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Note:National Aeronautics and Space Administration, 1959
  
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Subject:Aerodynamics, Supersonic -- Testing
Subject:Airplanes -- Models -- Propellers -- Testing
Subject:Fighter planes -- Testing
Subject:Heat -- Transmission -- Testing
Subject:Transonic wind tunnels -- Testing
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