Effects of Mach Number and Wall-temperature Ratio on Turbulent Heat Transfer at Mach Numbers from 3 to 5 PDF Download
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Author: Thorval Tendeland Publisher: ISBN: Category : Aerodynamic heating Languages : en Pages : 28
Book Description
The heat-transfer data obtained from the model were found to correlate when the T' method of Sommer and Short was used. The increase in turbulent heat-transfer rate with a reduction in wall to free-stream temperature ratio was of the same order of magnitude as has been found for the turbulent skin-friction coefficient.
Author: Thorval Tendeland Publisher: ISBN: Category : Aerodynamic heating Languages : en Pages : 28
Book Description
The heat-transfer data obtained from the model were found to correlate when the T' method of Sommer and Short was used. The increase in turbulent heat-transfer rate with a reduction in wall to free-stream temperature ratio was of the same order of magnitude as has been found for the turbulent skin-friction coefficient.
Author: Thorval Tendeland
Author: Thorval Tendeland
Author: Thorval Tendeland
Author: United States. National Advisory Committee for Aeronautics
Author: 
Author: Thorval Tendeland
Author: United States. Dept. of Commerce. Office of Technical Services
Author: 
Author: United States. National Advisory Committee for Aeronautics
Author: 
Author: United States. National Advisory Committee for Aeronautics