Supersonic Free Flight Measurement Of Heat Transfer And Transition On A 10 Degree Cone Having A Low Temperature Ratio
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Language: en
Pages: 28
Pages: 28
Type: BOOK - Published: 1961 - Publisher:
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-
Language: en
Pages: 24
Pages: 24
Type: BOOK - Published: 1957 - Publisher:
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
Language: en
Pages: 24
Pages: 24
Type: BOOK - Published: 1961 - Publisher:
Language: en
Pages: 42
Pages: 42
Type: BOOK - Published: 1956 - Publisher:
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
Language: en
Pages: 448
Pages: 448
Type: BOOK - Published: 1960 - Publisher: