Velocity Profile Skin Friction Balance And Heat Transfer Measurements Of The Turbulent Boundary Layers At Mach 5 And Zero Pressure Gradient
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Velocity Profile Skin Friction Balance And Heat Transfer Measurements Of The Turbulent Boundary Layers At Mach 5 And Zero Pressure Gradient
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Author : Roland E. Lee
language : en
Publisher:
Release Date : 1969
Velocity Profile Skin Friction Balance And Heat Transfer Measurements Of The Turbulent Boundary Layers At Mach 5 And Zero Pressure Gradient written by Roland E. Lee 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.
The results of a detailed experimental investigation of a two- dimensional turbulent boundary layer at zero-pressure gradient are presented. The studies were made at the free-stream Mach number of 5, momentum-thickness Reynolds number from 4800 to 56,000 and wall-to-adiabatic-wall temperature ratios from 0.5 to 1.0. The data are in analytical terms of velocity profile, temperature profile, law-of-the-wall, velocity-defect law and incompressible form factor. Comparisons of local skin-friction coefficients obtained by four different experimental methods are shown. An empirical equation was derived from the shear-balance data to calculate the friction coefficient from known values of Mach number, heat transfer and Reynolds number.
Skin Friction Measurements In Incompressible Flow
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Author : Donald W. Smith
language : en
Publisher:
Release Date : 1959
Skin Friction Measurements In Incompressible Flow written by Donald W. Smith and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Compressibility categories.
Experiment have been conducted to measure the local surface-shear stress and the average skin-friction coefficient in incompressible flow for a turbulent boundary layer on a smooth flat plate having zero pressure gradient. Data were obtained for a range of Reynolds numbers from 1 million to 45 million. The local surface-shear stress was measured by a floating-element skin-friction balance and also by a calibrated total head tube located on the surface of the test wall. The average skin-friction coefficient was obtained from boundary-layer velocity profiles.
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).
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.
Flow Visualization Studies Of A Fin Protuberance Partially Immersed In A Turbulent Boundary Layer At Mach 5
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Author : Allen Edward Winkelmann
language : en
Publisher:
Release Date : 1970
Flow Visualization Studies Of A Fin Protuberance Partially Immersed In A Turbulent Boundary Layer At Mach 5 written by Allen Edward Winkelmann and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Flow visualization categories.
Various flow-visualization results are presented for a cylindrically blunted, unswept fin (yawed and unyawed) partially immersed in a turbulent boundary layer (delta approx. = 2.6 inches). The model, consisting of a fin-flat plate combination, was tested at a nominal Mach number of 5 and nominal free-stream Reynolds numbers per foot of 2800 000 and 7400 000. Azobenzene tests show regions of high heat transfer on the flat plate immediately upstream and downstream of the fin. Oil smear tests show in detail the surface shear directions and locations of separated flow which occur on the model. Schlieren and shadowgraph photographs indicate the complex shock wave structure which exists in front of the fin. A possible flow-field model is suggested to account for the observed flow patterns. (Author).
Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1972
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 1972 with categories.
A Review Of Turbulence Measurements In Compressible Flow
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Author : Virgil A. Sandborn
language : en
Publisher:
Release Date : 1974
A Review Of Turbulence Measurements In Compressible Flow written by Virgil A. Sandborn and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Fluid dynamics categories.
Compressible Turbulent Boundary Layers
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Author :
language : en
Publisher:
Release Date : 1969
Compressible Turbulent Boundary Layers written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Compressibility categories.
Comparison Of Prediction Methods And Studies Of Relaxation In Hypersonic Turbulent Nozzle Wall Boundary Layers
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Author : Dennis M. Bushnell
language : en
Publisher:
Release Date : 1969
Comparison Of Prediction Methods And Studies Of Relaxation In Hypersonic Turbulent Nozzle Wall Boundary Layers written by Dennis M. Bushnell 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, Hypersonic categories.
Turbulent boundary layer measurements on axisymmetric hypersonic nozzle walls.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1994
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Aeronautics categories.