3,017 research outputs found
Heat-Transfer and Pressure Measurements from a Flight Test of a 1/18-Scale Model of the Titan Intercontinental Ballistic Missile up to a Mach Number of 3.95 and Reynolds Number Per Foot of 23 by 10 to the 6Th Power
Get PDFTemperature Measurements from a Flight Test of Two Wing-body Combinations at 7 Degree Angle of Attack for Mach Numbers to 4.86 and Reynolds Numbers to 19.2 X 10(exp 6)
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Pressure Distribution and Pressure Drag for a Hemispherical Nose at Mach Numbers 2.05, 2.54, and 3.04
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Aerodynamic Heat Transfer and Zero-lift Drag of a Flat Windshield Canopy on the NACA RM-10 Research Vehicle at High Reynolds Numbers for a Flight Mach Number Range from 1.5 to 3.0
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Correlation of Supersonic Convective Heat-transfer Coefficients from Measurements of the Skin Temperature of a Parabolic Body of Revolution (NACA RM-10)
Get PDFCorrelation of Supersonic Convective Heat-transfer Coefficients from Measurements of the Skin Temperature of a Parabolic Body of Revolution (NACA RM-10)
Get PDFExperimental convective heat transfer to a 4-inch and 6-inch hemisphere at Mach numbers from 1.62 to 3.04
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