Analysis Of The Three Dimensional Compressible Turbulent Boundary Layer On A Sharp Cone At Incidence In Supersonic And Hypersonic Flow
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Analysis Of The Three Dimensional Compressible Turbulent Boundary Layer On A Sharp Cone At Incidence In Supersonic And Hypersonic Flow
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Author : John C. Adams
language : en
Publisher:
Release Date : 1972
Analysis Of The Three Dimensional Compressible Turbulent Boundary Layer On A Sharp Cone At Incidence In Supersonic And Hypersonic Flow written by John C. Adams and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Aerodynamics, Hypersonic categories.
An analytical approach toward numerical calculation of the three-dimensional turbulent boundary layer on a sharp cone at incidence under supersonic and hypersonic flow conditions is presented. The theoretical model is based on implicit finite-difference integration of the governing three-dimensional turbulent boundary-layer equations in conjunction with a three-dimensional scalar eddy-viscosity model of turbulence. Comparison is made of present theory with detailed experimental measurements of the three-dimensional turbulent boundary-layer structure (velocity and temperature profiles), the surface streamline direction (obtained via an oil-flow technique) and surface heat-transfer rate.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1987
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 1987 with Aeronautics categories.
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Applied Mechanics Reviews
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Author :
language : en
Publisher:
Release Date : 1973
Applied Mechanics Reviews 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 Mechanics, Applied categories.
Heat Transfer And Flow Field Tests Of The Mcdonnell Douglas Martin Marietta Space Shuttle Configurations
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Author : Richard K. Matthews
language : en
Publisher:
Release Date : 1973
Heat Transfer And Flow Field Tests Of The Mcdonnell Douglas Martin Marietta Space Shuttle Configurations written by Richard K. Matthews and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Aerothermodynamics categories.
Aerothermodynamic tests of Phase B space shuttle configurations proposed by McDonnell Douglas--Martin Marietta were conducted at Mach numbers 8 and 10.5. Test conditions provided both Mach number and Reynolds number simulation for typical ascent and reentry trajectories. This report provides a comprehensive analysis of the major test results and also presents data comparisons with theoretical calculations. Specific areas covered are ascent heating and shock interference, booster reentry heating and flow fields, and orbiter reentry analysis which includes leeside heating, windward shock angles and flow fields, windward surface heating, and boundary-layer transition.
Nasa Sp
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Author :
language : en
Publisher:
Release Date : 1962
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 1962 with Aeronautics categories.
Analysis Of The Three Dimensional Compressible Turbulent Boundary Layer On A Sharp Cone At Incidence In Supersonic And Hypersonic Flow
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1972
Analysis Of The Three Dimensional Compressible Turbulent Boundary Layer On A Sharp Cone At Incidence In Supersonic And Hypersonic Flow 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.
An analytical approach toward numerical calculation of the three-dimensional turbulent boundary layer on a sharp cone at incidence under supersonic and hypersonic flow conditions is presented. The theoretical model is based on implicit finite-difference integration of the governing three-dimensional turbulent boundary-layer equations in conjunction with a three-dimensional scalar eddy-viscosity model of turbulence. Comparison is made of present theory with detailed experimental measurements of the three-dimensional turbulent boundary-layer structure (velocity and temperature profiles), the surface streamline direction (obtained via an oil-flow technique) and surface heat-transfer rate.
Analysis Of The Three Dimensional Compressible Turbulent Boundary Layer On A Sharp Cone At Incidence In Supersonic And Hypersonic Flow
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1972
Analysis Of The Three Dimensional Compressible Turbulent Boundary Layer On A Sharp Cone At Incidence In Supersonic And Hypersonic Flow 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.
An analytical approach toward numerical calculation of the three-dimensional turbulent boundary layer on a sharp cone at incidence under supersonic and hypersonic flow conditions is presented. The theoretical model is based on implicit finite-difference integration of the governing three-dimensional turbulent boundary-layer equations in conjunction with a three-dimensional scalar eddy-viscosity model of turbulence. Comparison is made of present theory with detailed experimental measurements of the three-dimensional turbulent boundary-layer structure (velocity and temperature profiles), the surface streamline direction (obtained via an oil-flow technique) and surface heat-transfer rate.
Aiaa 73 622 Aiaa 73 658
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Author :
language : en
Publisher:
Release Date : 1973
Aiaa 73 622 Aiaa 73 658 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 Fluid dynamics categories.
Wall Temperature Effects On Two And Three Dimensional Transonic Turbulent Boundary Layers
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Author : J. C Adams (Jr.)
language : en
Publisher:
Release Date : 1973
Wall Temperature Effects On Two And Three Dimensional Transonic Turbulent Boundary Layers written by J. C Adams (Jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Space vehicles categories.
Wall temperature effects on two- and three-dimensional high Reynolds number turbulent boundary layers are examined for representative high Reynolds number tunnel (HIRT) conditions relative to flight; also considered are hot-wall conditions relative to space shuttle subsonic and transonic flight during earth entry. Results show significant influences of wall-to-stagnation temperature ratio on the location of boundary-layer separation and the friction drag coefficient. The study also indicates how rapid model wall temperature during a typical testing period of 2 to 10 sec may be undesirable for HIRT testing since unsteady aerodynamic phenomena can be influenced by rapidly changing turbulent boundary-layer wall temperature levels. (Modified author abstract).
A Collection Of Technical Papers
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Author :
language : en
Publisher:
Release Date : 1975
A Collection Of Technical Papers written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Fluid dynamics categories.