FREE-FLIGHT AERODYNAMIC-HEATING DATA TO MACH NUMBER 10.4 FOR A MODIFIED VON KARMAN NOSE SHAPE.
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Published: 1961
Total Pages: 32
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Published: 1961
Total Pages: 32
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DOWNLOAD EBOOKAuthor: William M. Bland
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Published: 1956
Total Pages: 28
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DOWNLOAD EBOOKAuthor: William M. Bland
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Published: 1961
Total Pages: 28
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DOWNLOAD EBOOKAuthor: William M. Bland
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Published: 1961
Total Pages: 28
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DOWNLOAD EBOOKAuthor: Charles Bertrand Rumsey
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Published: 1960
Total Pages: 30
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DOWNLOAD EBOOKAuthor: Charles B. Rumsey
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Published: 1955
Total Pages: 26
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DOWNLOAD EBOOKAerodynamic-heat-transfer measurements have been made at a station on the 10 degree total angle conical nose of a rocket-propelled model at flight Mach numbers of 1.4 to 3.9. The corresponding values of local Reynolds number varied from 18,000,000 to 46,000,000 and the ratio of skin temperature to local static temperature varied from 1.2 to 2.4. The experimental data, reduced to Stanton number, were in fair agreement with values predicted by Van Driest's theory for heat transfer on a cone with turbulent flow from the nose tip.
Author: Charles B. Rumsey
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Published: 1958
Total Pages: 50
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DOWNLOAD EBOOKAuthor: William M. Bland
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Published: 1957
Total Pages: 42
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DOWNLOAD EBOOKAuthor: Benjamine J. Garland
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Published: 1962
Total Pages: 36
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DOWNLOAD EBOOKAuthor:
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Published: 1961
Total Pages: 986
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