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Heat Transfer To Boundary Layers With Pressure Gradients


Heat Transfer To Boundary Layers With Pressure Gradients
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Heat Transfer To Boundary Layers With Pressure Gradients


Heat Transfer To Boundary Layers With Pressure Gradients
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Author : Ralph Alois Seban
language : en
Publisher:
Release Date : 1958

Heat Transfer To Boundary Layers With Pressure Gradients written by Ralph Alois Seban and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Boundary layer categories.




Heat Transfer To Boundary Layers With Pressure Gradients


Heat Transfer To Boundary Layers With Pressure Gradients
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Author : Ralph Alois Seban
language : en
Publisher:
Release Date : 1957

Heat Transfer To Boundary Layers With Pressure Gradients written by Ralph Alois Seban and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aerothermodynamics categories.




Heat Transfer Across Turbulent Boundary Layers With Pressure Gradients


Heat Transfer Across Turbulent Boundary Layers With Pressure Gradients
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Author : Yaning Lu
language : en
Publisher:
Release Date : 1987

Heat Transfer Across Turbulent Boundary Layers With Pressure Gradients written by Yaning Lu and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1987 with Heat categories.




Heat Transfer To Turbulent Boundary Layers In Pressure Gradients


Heat Transfer To Turbulent Boundary Layers In Pressure Gradients
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Author : John Boyd Bell
language : en
Publisher:
Release Date : 1966

Heat Transfer To Turbulent Boundary Layers In Pressure Gradients written by John Boyd Bell and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Turbulent boundary layer categories.




Calculation Of Compressible Turbulent Boundary Layers With Pressure Gradients And Heat Transfer


Calculation Of Compressible Turbulent Boundary Layers With Pressure Gradients And Heat Transfer
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Author : Larry L. Lynes
language : en
Publisher:
Release Date : 1969

Calculation Of Compressible Turbulent Boundary Layers With Pressure Gradients And Heat Transfer written by Larry L. Lynes and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Air flow categories.




The Effect Of Pressure Gradients On Transition Zone Length In Hypersonic Boundary Layers


The Effect Of Pressure Gradients On Transition Zone Length In Hypersonic Boundary Layers
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Author : Roger L. Kimmel
language : en
Publisher:
Release Date : 1993

The Effect Of Pressure Gradients On Transition Zone Length In Hypersonic Boundary Layers written by Roger L. Kimmel and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with Aerodynamics, Hypersonic categories.


Boundary layer transition was measured in zero, favorable, and adverse pressure gradients at Mach 8 using heat transfer. Models consisted of 7 degrees half angle forecones 0.4826 m long, followed by flared or ogive aft bodies 0.5334 m long. The flares and ogives produced constant pressure gradients. For the cases examined, favorable pressure gradients delay transition and adverse pressure gradients promote transition, but transition zone lengths are shorter in favorable pressure gradient. Results of the effect of adverse pressure gradient on transition zone lengths were inconclusive.



Experimental Investigation Of Turbulent Boundary Layers With Pressure Gradient And Heat Transfer At Mach Number 4


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).



An Investigation Of The High Speed Turbulent Boundary Layer With Heat Transfer And Arbitrary Pressure Gradient The Compressibility Transformation


An Investigation Of The High Speed Turbulent Boundary Layer With Heat Transfer And Arbitrary Pressure Gradient The Compressibility Transformation
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Author : Constantino Economos
language : en
Publisher:
Release Date : 1970

An Investigation Of The High Speed Turbulent Boundary Layer With Heat Transfer And Arbitrary Pressure Gradient The Compressibility Transformation written by Constantino Economos and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Heat categories.


This report investigates the behavior of high speed turbulent boundary layer with heat transfer and streamwise pressure gradient.



Method For Predicting Compressible Turbulent Boundary Layers In Adverse Pressure Gradients


Method For Predicting Compressible Turbulent Boundary Layers In Adverse Pressure Gradients
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Author : Shimer Zane Pinckney
language : en
Publisher:
Release Date : 1971

Method For Predicting Compressible Turbulent Boundary Layers In Adverse Pressure Gradients written by Shimer Zane Pinckney and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Boundary layer categories.




An Investigation Of The High Speed Turbulent Boundary Layer With Heat Transfer And Arbitrary Pressure Gradient Part 2 The Compressibility Transformation General Considerations


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.