Author: John L. Allen
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 80
Book Description
Base Heat Transfer, Pressure Ratios, and Configuration Effects Obtained on a 1/27 Scall Saturn (C-1) Model at Mach Numbers from 0.1 to 2.0
Base Heat Transfer, Pressure Ratios and Configuration Effects Obtained on a 1/27 Scale Saturn (C-1) Model at Mach Numbers from 0.1 to 2.0
Base Heat Transfer, Pressure Ratios, and Configuration Effects Obtained on a 1/27 Scall Saturn (C-1) Model at Mach Numbers from 0.1 to 2.0
Base Heat Transfer, Pressure Rations and Configuration Effects Obtained on a 1/27 Scale Saturn (C-1) Model at MAch Numbers from 0.1 to 2.0
Scientific and Technical Aerospace Reports
Journal of the Royal Aeronautical Society
Applied Mechanics Reviews
Effects of Mach Number and Wall-temperature Ratio on Turbulent Heat Transfer at Mach Numbers from 3 to 5
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.
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.
Laminar Heat-transfer Distributions for a Blunted-cone, Cone-frustum Reentry Configuration at Mach 10
Author: J. David Dearing
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 28
Book Description