Heat Transfer for Mach Numbers up to 2.2 and Pressure Distributions for Mach Numbers up to 4.7 from Flight Investigations of a Flat-face-cone and a Hemisphere-cone
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Speegle, Katherine C↗
Engineering topics
Chauvin, Leo T
Publications and source records attributed to Chauvin, Leo T.
Temperature 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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Chauvin, Leo T↗
Flight Measurements of Boundary-layer Temperature Profiles on a Body of Revolution (NACA RM-10) at Mach Numbers from 1.2 to 3.5
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Swanson, Andrew G↗
Measurement of Aerodynamic Heat Transfer to a Deflected Trailing-edge Flap on a Delta Fin in Free Flight at Mach Numbers from 1.5 to 2.6
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Chauvin, Leo T↗
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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Hoffman, Sherwood↗
Correlation of Supersonic Convective Heat-transfer Coefficients from Measurements of the Skin Temperature of a Parabolic Body of Revolution (NACA RM-10)
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Chauvin, Leo T↗
Aerodynamic heating of aircraft components
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Chauvin, Leo T↗
Aerodynamic heating of aircraft components
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Chauvin, Leo T↗
Exploratory Tests of Transpiration Cooling on a Porous 8 Degree Cone at M = 2.05 Using Nitrogen Gas, Helium Gas, and Water as the Coolants
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Chauvin, Leo T↗
Turbulent Convective Heat-transfer Coefficients Measured from Flight Tests of Four Research Models (NACA RM-10) at Mach Numbers from 1.0 to 3.6
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Chauvin, Leo T↗
Flight Measurements of Drag and Base Pressure of a Fin-stabilized Parabolic Body of Revolution (NACA RM-10) at Different Reynolds Numbers and at Mach Numbers from 0.9 to 3.3
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Jackson, H Herbert↗
Experimental convective heat transfer to a 4-inch and 6-inch hemisphere at Mach numbers from 1.62 to 3.04
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Chauvin, Leo T↗
Exploratory Investigation of Transpiration Cooling to Alleviate Aerodynamic Heating on an 8 Degree Cone in a Free Jet at a Mach Number of 2.05
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O'Sullivan, William J↗
Pressure Distribution and Pressure Drag for a Hemispherical Nose at Mach Numbers 2.05, 2.54, and 3.04
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Chauvin, Leo T↗
Correlation of Supersonic Convective Heat-transfer Coefficients from Measurements of the Skin Temperature of a Parabolic Body of Revolution (NACA RM-10)
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Chauvin, Leo T↗
Flight measurements of drag and base pressure of a fin-stabilized parabolic body of revolution (NACA RM-10) at different Reynolds numbers and at Mach numbers from 0.9 to 3.3
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Jackson, H Herbert↗
Flight Tests to Determine the Drag of Fin-stabilized Parabolic Bodies at Transonic and Supersonic Speeds
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Alexander, Sidney R↗