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Author:
Publisher: Academic Press
ISBN: 0080575706
Category : Science
Languages : en
Pages : 401
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Book Description
Advances in Heat Transfer
Author:
Publisher: Academic Press
ISBN: 0080575706
Category : Science
Languages : en
Pages : 401
Get Book Here
Book Description
Advances in Heat Transfer
Author: Stanford University. Thermosciences Division. Thermosciences Division
Publisher:
ISBN:
Category : Cooling
Languages : en
Pages : 122
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
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Book Description
Author: Stanford University. Thermosciences Division. Thermosciences Division
Publisher:
ISBN:
Category :
Languages : en
Pages : 178
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Book Description
Author: Stanford University. Thermosciences Division. Thermosciences Division
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 232
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Book Description
Author: Stanford University. Thermosciences Division. Thermosciences Division
Publisher:
ISBN:
Category :
Languages : en
Pages : 170
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Book Description
Author: H. K. Kim
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 164
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Book Description
An experimental study of heat transfer was conducted on a turbulent boundary layer with full-coverage film cooling through an array of holes inclined at 30 degrees to the surface and 45 degrees to the flow direction.
Author: Raymond Strong Colladay
Publisher:
ISBN:
Category : Cooling
Languages : en
Pages : 52
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Book Description
The relative performance of (1) counterflow film cooling, (2) parallel-flow film cooling, (3) convection cooling, (4) adiabatic film cooling, (5) transpiration cooling, and (6) full-coverage film cooling was investigated for heat loading conditions expected in future gas turbine engines. Assumed in the analysis were hot-gas conditions of 2200 K (3500 F) recovery temperature, 5 to 40 atmospheres total pressure, and 0.6 gas Mach number and a cooling air supply temperature of 811 K (1000 F). The first three cooling methods involve film cooling from slots. Counterflow and parallel flow describe the direction of convection cooling air along the inside surface of the wall relative to the main gas flow direction. The importance of utilizing the heat sink available in the coolant for convection cooling prior to film injection is illustrated.
Author: Stanford University. Thermosciences Division. Thermosciences Division
Publisher:
ISBN:
Category :
Languages : en
Pages : 126
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Book Description
Author: Stanford University. Thermosciences Division. Thermosciences Division
Publisher:
ISBN:
Category :
Languages : en
Pages : 96
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Book Description
The present study is an extension of the previous work of the Heat and Mass Transfer Group at Stanford on adverse pressure gradient turbulent boundary layers. The objective here is to acquire hydrodynamic and heat transfer data for.
