Summary And Correlation Of Skin Friction And Heat Transfer Data For A Hypersonic Turbulent Boundary Layer On Simple Shapes
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Summary And Correlation Of Skin Friction And Heat Transfer Data For A Hypersonic Turbulent Boundary Layer On Simple Shapes
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Author : Edward J. Hopkins
language : en
Publisher:
Release Date : 1969
Summary And Correlation Of Skin Friction And Heat Transfer Data For A Hypersonic Turbulent Boundary Layer On Simple Shapes written by Edward J. Hopkins and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Cone categories.
Skin friction and heat transfer data for hypersonic turbulent layer on flat plates, wind tunnel wall, and cones.
A Correlation Of Heat Transfer And Skin Friction Data And An Experimental Reynolds Analogy Factor For Highly Cooled Turbulent Boundary Layers At Mach 5 0
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Author : Donald M. Wilson
language : en
Publisher:
Release Date : 1969
A Correlation Of Heat Transfer And Skin Friction Data And An Experimental Reynolds Analogy Factor For Highly Cooled Turbulent Boundary Layers At Mach 5 0 written by Donald M. Wilson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Heat categories.
Turbulent boundary-layer heat transfer and skin-friction coefficients were measured on sharp slender cones at a free-stream Mach number of 5.0. Wall-to-stagnation temperature ratios from 0.15 to 0.80 were obtained by precooling or preheating the model. Tests were conducted for a wide range of Reynolds numbers by varying the tunnel supply pressure and temperature, thus providing data for naturally turbulent boundary layers. The experimental results were compared with existing theories which predict convective Stanton number or skin-friction coefficients. These comparisons indicate that the heat-transfer data are best predicted by the Spalding-Chi law and the skin friction by the Sommer-Short reference temperature method. The experimental Reynolds analogy factor is adequately predicted by Colburn's incompressible correlation for wall-to-stagnation temperature ratios above about 0.5. However, for lower wall temperature ratios, the experimental Reynolds analogy factor decreases with decreased temperature ratios in a manner which has not been previously reported. (Author).
Use Of Preston Tubes For Measuring Hypersonic Turbulent Skin Friction
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Author : Earl R. Keener
language : en
Publisher:
Release Date : 1969
Use Of Preston Tubes For Measuring Hypersonic Turbulent Skin Friction written by Earl R. Keener and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Aerodynamics, Supersonic categories.
Use of Preston tubes for measuring hypersonic turbulent skin friction.
Analytical Numerical And Experimental Results On Turbulent Boundary Layers
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Author : David L. Whitfield
language : en
Publisher:
Release Date : 1976
Analytical Numerical And Experimental Results On Turbulent Boundary Layers written by David L. Whitfield and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with Laminar boundary layer categories.
This report describes the results of analytical, numerical, and experimental investigations of incompressible and compressible boundary layers. The subjects considered are (1) Laminar and/or turbulent numerical boundary-layer calculations in which the Reynolds stress is related to the turbulent kinetic energy; (2) an analytical investigation of turbulence near a wall which is not founded on classical mixing-length theory; (3) analytical solutions for relating velocity and temperature throughout turbulent boundary layers for nonunity Prandtl numbers; (4) a description of the data reduction of pitot pressure measurements utilizing these analytical results, and (5) the application of the numerical and analytical results to the analysis of turbulent boundary-layer measurements made in the Propulsion Wind Tunnel Facility (PWT).
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.
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.
Aerothermodynamics Of Aircraft Engine Components
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Author : Gordon C. Oates
language : en
Publisher: AIAA
Release Date : 1985
Aerothermodynamics Of Aircraft Engine Components written by Gordon C. Oates and has been published by AIAA this book supported file pdf, txt, epub, kindle and other format this book has been release on 1985 with Aerothermodynamics categories.
Annotation Design and R & D engineers and students will value the comprehensive, meticulous coverage in this volume. Beginning with the basic principles and concepts of aeropropulsion combustion, chapters explore specific processes, limitations, and analytical methods as they bear on component design.
Direct Measurements Of Turbulent Skin Friction On A Nonadiabatic Flat Plate At Mach Number 6 5 And Comparisons With Eight Theories
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Author : Edward J. Hopkins
language : en
Publisher:
Release Date : 1970
Direct Measurements Of Turbulent Skin Friction On A Nonadiabatic Flat Plate At Mach Number 6 5 And Comparisons With Eight Theories written by Edward J. Hopkins and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Aerodynamics, Hypersonic 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.
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.