The Turbulent Boundary Layer Experimental Heat Transfer With Strong Favorable Pressure Gradients And Blowing
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The Turbulent Boundary Layer Experimental Heat Transfer With Strong Favorable Pressure Gradients And Blowing
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Author : Stanford University. Thermosciences Division. Thermosciences Division
language : en
Publisher:
Release Date : 1970
The Turbulent Boundary Layer Experimental Heat Transfer With Strong Favorable Pressure Gradients And Blowing written by Stanford University. Thermosciences Division. Thermosciences Division and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Boundary layer categories.
Turbulent Boundary Layer Experimental Heat Transfer With Blowing Suction And Favorable Pressure Gradient
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Author : Stanford University. Thermosciences Division
language : en
Publisher:
Release Date : 1969
Turbulent Boundary Layer Experimental Heat Transfer With Blowing Suction And Favorable Pressure Gradient written by Stanford University. Thermosciences Division and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with categories.
The Turbulent Boundary Layer
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Author : William Holmes Thielbahr
language : en
Publisher:
Release Date : 1969
The Turbulent Boundary Layer written by William Holmes Thielbahr and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Boundary layer categories.
The Turbulent Boundary Layer On A Porous Plate An Experimental Study Of The Fluid Dynamics With Strong Favorable Pressure Gradients And Blowing
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Author : Robert Jackson Loyd
language : en
Publisher:
Release Date : 1970
The Turbulent Boundary Layer On A Porous Plate An Experimental Study Of The Fluid Dynamics With Strong Favorable Pressure Gradients And Blowing written by Robert Jackson Loyd and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Boundary layer categories.
Behavior Of Transpired Turbulent Boundary Layers
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Author : Stanford University. Thermosciences Division. Thermosciences Division
language : en
Publisher:
Release Date : 1975
Behavior Of Transpired Turbulent Boundary Layers written by Stanford University. Thermosciences Division. Thermosciences Division and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with categories.
Heat Transfer To The Transpired Turbulent Boundary Layer
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Author : Stanford University. Thermosciences Division. Thermosciences Division
language : en
Publisher:
Release Date : 1971
Heat Transfer To The Transpired Turbulent Boundary Layer written by Stanford University. Thermosciences Division. Thermosciences Division and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Cooling categories.
Examination Of The Existing Data On The Heat Transfer Of Turbulent Boundary Layers At Supersonic Speeds From The Point Of View Of Reynolds Analogy
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Author : Alvin Seiff
language : en
Publisher:
Release Date : 1954
Examination Of The Existing Data On The Heat Transfer Of Turbulent Boundary Layers At Supersonic Speeds From The Point Of View Of Reynolds Analogy written by Alvin Seiff and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aerodynamics, Supersonic categories.
Heat-transfer data from four wind-tunnel experiments and two free-flight experiments with turbulent boundary layers have been examined to see whether or not they are well represented by the Reynolds analogy or a modification thereof. The heat-transfer results are put into the form of dimensionless Stanton numbers based on fluid properties at the outer edge of the boundary layer and are compared with skin-friction coefficients for the same Mach numbers and wall to free-stream temperature ratios as obtained from an interpolation of the existing skin-friction data. The effective Reynolds number is taken to be the length Reynolds number measured from the effective turbulent origin, a position which differs importantly from the leading edge of the test surface in some cases.
An Investigation Of The High Speed Turbulent Boundary Layer With Heat Transfer And Arbitrary Pressure Gradient Part 2 The Compressibility Transformation General Considerations
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Author :
language : en
Publisher:
Release Date : 1970
An Investigation Of The High Speed Turbulent Boundary Layer With Heat Transfer And Arbitrary Pressure Gradient Part 2 The Compressibility Transformation General Considerations written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with categories.
Experimental Investigation Of Turbulent Boundary Layers With Pressure Gradient And Heat Transfer At Mach Number 4
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Author : J. S. Hahn
language : en
Publisher:
Release Date : 1971
Experimental Investigation Of Turbulent Boundary Layers With Pressure Gradient And Heat Transfer At Mach Number 4 written by J. S. Hahn and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with categories.
An experimental investigation of the behavior of a turbulent boundary layer subjected to adverse and favorable pressure gradients was conducted at Mach number 4 for a free-stream Reynolds number of 0.500,000 per inch. Two severe pressure gradients were imposed on the boundary layer by interchangeable contoured centerbodies inside a large hollow cylinder for cold-wall and adiabatic-wall temperature conditions. Imposition of either of the adverse pressure gradients significantly decreased the natural growth rate of the boundary-layer displacement thickness, whereas the favorable pressure gradient had opposite effects; momentum thickness was relatively unaffected by pressure gradient. A pressure gradient increase of about 30 percent caused relatively small changes in the skin friction, heat-transfer rate, and the characteristic boundary-layer parameters. Wall cooling effects (T sub w/t sub 0 approximately 0.3) on the boundary-layer thickness parameters were nearly insignificant, in comparison with the adiabatic-wall results. Heat-transfer distributions were similar to the local skin friction results based on free-stream conditions. (Author).
Turbulent Boundary Layer On A Porous Plate An Experiment Study Of The Heat Transfer Behavior With Adverse Pressure Gradients
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Author : Stanford University. Thermosciences Division. Thermosciences Division
language : en
Publisher:
Release Date : 1972
Turbulent Boundary Layer On A Porous Plate An Experiment Study Of The Heat Transfer Behavior With Adverse Pressure Gradients written by Stanford University. Thermosciences Division. Thermosciences Division and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with categories.