Summary Of Available Information On Reynolds Analogy For Zero Pressure Gradient Compressible Turbulent Boundary Layer Flow
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Summary Of Available Information On Reynolds Analogy For Zero Pressure Gradient Compressible Turbulent Boundary Layer Flow
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Author : Aubrey M. Cary
language : en
Publisher:
Release Date : 1970
Summary Of Available Information On Reynolds Analogy For Zero Pressure Gradient Compressible Turbulent Boundary Layer Flow written by Aubrey M. Cary and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Reynolds analogy categories.
Mathematical analysis of Reynolds analogy for turbulent heat transfer, skin friction, and boundary layer flow in adiabatic conditions.
Summary Of Available Information On Reynolds Analogy For Zero Pressure Gradient Compressible Turbulent Boundary Layer Flow
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Author : Aubrey M. Cary
language : en
Publisher:
Release Date : 1969
Summary Of Available Information On Reynolds Analogy For Zero Pressure Gradient Compressible Turbulent Boundary Layer Flow written by Aubrey M. Cary 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.
An Approximate Method For The Calculation Of The Reynolds Analogy Factor For A Compressible Turbulent Boundary Layer In A Pressure Gradient
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Author : Neal Tetervin
language : en
Publisher:
Release Date : 1967
An Approximate Method For The Calculation Of The Reynolds Analogy Factor For A Compressible Turbulent Boundary Layer In A Pressure Gradient written by Neal Tetervin and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Enthalpy categories.
The method predicts that a positive pressure gradient increases and a negative pressure gradient decreases the ratio of Stanton number to friction coefficient. The Crocco relation between the velocity and total enthalpy for a non-adiabatic surface and zero pressure gradient is generalized to non-zero pressure gradient. The relation between the velocity and the total enthalpy varies markedly from the flat plate Crocco relation as the pressure gradient departs from zero. The magnitude of the variation depends on the velocity profile shape parameter. (Author).
Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1973
Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with categories.
An Approximate Method For The Calculation Of The Reynolds Analogy Factor For A Compressible Turbulent Boundary Layer In A Pressure Gradient
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Author : Neal Tetervin
language : en
Publisher:
Release Date : 1967
An Approximate Method For The Calculation Of The Reynolds Analogy Factor For A Compressible Turbulent Boundary Layer In A Pressure Gradient written by Neal Tetervin and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with categories.
The method predicts that a positive pressure gradient increases and a negative pressure gradient decreases the ratio of Stanton number to friction coefficient. The Crocco relation between the velocity and total enthalpy for a non-adiabatic surface and zero pressure gradient is generalized to non-zero pressure gradient. The relation between the velocity and the total enthalpy varies markedly from the flat plate Crocco relation as the pressure gradient departs from zero. The magnitude of the variation depends on the velocity profile shape parameter. (Author).
Measurements Of A Mach 4 9 Zero Pressure Gradient Turbulent Boundary Layer With Heat Yransfer
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Author : Robert L. P. Voisinet
language : en
Publisher:
Release Date : 1972
Measurements Of A Mach 4 9 Zero Pressure Gradient Turbulent Boundary Layer With Heat Yransfer written by Robert L. P. Voisinet and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Heat categories.
The results of a detailed experimental investigation of the compressible turbulent boundary layer in a zero-pressure-gradient flow are presented for zero, moderate and severe heat-transfer conditions. The studies were conducted on a flat nozzle wall for a nominal Mach number of 4.9, at momentum thickness Reynolds numbers from 7,000. to 58,000. and at wall-to-adiabatic-wall temperature ratios of 1.0, 0.8 and 0.25. Complete profile measurements were taken with Pitot pressure probes and conical-equilibrium and fine-wire temperature probes. Furthermore, the wall shear and surface heat transfer were measured directly with a skin-friction balance and a heat-transfer gage, respectively. (Author Modified Abstract).
Monthly Catalog Of United States Government Publications Cumulative Index
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Author : United States. Superintendent of Documents
language : en
Publisher:
Release Date : 1979
Monthly Catalog Of United States Government Publications Cumulative Index written by United States. Superintendent of Documents and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with United States categories.
Nasa Sp
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Author :
language : en
Publisher:
Release Date : 1970
Nasa Sp 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 Aeronautics categories.
Turbulent Boundary Layer Heat Transfer And Transition Measurements With Surface Cooling At Mach 6
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Author : Aubrey M. Cary
language : en
Publisher:
Release Date : 1970
Turbulent Boundary Layer Heat Transfer And Transition Measurements With Surface Cooling At Mach 6 written by Aubrey M. Cary 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.
Nasa Technical Paper
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Author :
language : en
Publisher:
Release Date : 1980
Nasa Technical Paper written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Science categories.