Supersonic Free Flight Measurement Of Heat Transfer And Transition On A 10 Degree Cone Having A Low Temperature Ratio

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Supersonic Free-flight Measurements of Heat Transfer and Transition on a 10° Cone Having a Low Temperature Ratio
Language: en
Pages: 28
Authors: Charles F. Merlet
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1961 - Publisher:

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Heat-transfer coefficients in the form of Stanton number and boundary-layer transition data were obtained from a free-flight test of a 100-inch-long 10° total-
Supersonic Free-flight Measurement of Heat Transfer and Transition on a 10 Degree Cone Having a Low Temperature Ratio
Language: en
Pages: 24
Authors: Charles F. Merlet
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1957 - Publisher:

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Heat-transfer coefficients in the form of Stanton number and boundary-layer transition data were obtained from a free-flight test of a 100-inch-long 10 degree t
Supersonic Free-flight Measurement of Heat Transfer and Transition on a 10° Cone Having a Low Temperature Ratio
Language: en
Pages: 24
Measurements of Aerodynamic Heat Transfer and Boundary-layer Transition on a 10° Cone in Free Flight at Supersonic Mach Numbers Up to 5.9
Language: en
Pages: 42
Authors: Charles B. Rumsey
Categories: Aerodynamics
Type: BOOK - Published: 1956 - Publisher:

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Abstract: Aerodynamic heat-transfer measurements were at six stations on the 40-inch-long 10° total-angle conical nose of a rocket-propelled model which was fl
Index of NASA Technical Publications
Language: en
Pages: 448
Authors: United States. National Aeronautics and Space Administration
Categories: Aeronautics
Type: BOOK - Published: 1960 - Publisher:

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