Analysis Of The Three Dimensional Compressible Turbulent Boundary Layer On A Sharp Cone At Incidence In Supersonic And Hypersonic Flow
Download and Read Analysis Of The Three Dimensional Compressible Turbulent Boundary Layer On A Sharp Cone At Incidence In Supersonic And Hypersonic Flow full books in PDF, ePUB, and Kindle. Read online free Analysis Of The Three Dimensional Compressible Turbulent Boundary Layer On A Sharp Cone At Incidence In Supersonic And Hypersonic Flow ebook anywhere anytime directly on your device. We cannot guarantee that every ebooks is available!
Author | : John C. Adams |
Publisher | : |
Total Pages | : 98 |
Release | : 1972 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download Analysis of the Three-dimensional Compressible Turbulent Boundary Layer on a Sharp Cone at Incidence in Supersonic and Hypersonic Flow Book in PDF, Epub and Kindle
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.
Author | : |
Publisher | : |
Total Pages | : 0 |
Release | : 1972 |
Genre | : |
ISBN | : |
Download Analysis of the Three-Dimensional Compressible Turbulent Boundary Layer on a Sharp Cone at Incidence in Supersonic and Hypersonic Flow Book in PDF, Epub and Kindle
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.
Author | : |
Publisher | : |
Total Pages | : 0 |
Release | : 1972 |
Genre | : |
ISBN | : |
Download Analysis of the Three-Dimensional Compressible Turbulent Boundary Layer on a Sharp Cone at Incidence in Supersonic and Hypersonic Flow Book in PDF, Epub and Kindle
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.
Author | : John C. Adams (Jr.) |
Publisher | : |
Total Pages | : 124 |
Release | : 1971 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download Three-dimensional Laminar Boundary-layer Analysis of Upwash Patterns and Entrained Vortex Formation on Sharp Cones at Angle of Attack Book in PDF, Epub and Kindle
Application of three-dimensional inviscid and viscous (laminar boundary layer) analyses for cold wall hypersonic flows over sharp cones at incidence is presented relative to experimental data, showing surface upwash angles and entrained vortex formation leading to crossflow-induced boundary-layer transition. Three-dimensional neutral inviscid stability theory for stationary disturbances is used to calculate the angular orientation of the entrained vortices in the boundary layer while a maximum crossflow Reynolds number concept is applied for correlation of the onset to vortex formation due to crossflow instability.
Author | : |
Publisher | : |
Total Pages | : 1126 |
Release | : 1987 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, Epub and Kindle
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.
Author | : |
Publisher | : |
Total Pages | : 788 |
Release | : 1975 |
Genre | : Aerodynamics |
ISBN | : |
Download Aerodynamic Analyses Requiring Advanced Computers Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 724 |
Release | : 1962 |
Genre | : Aeronautics |
ISBN | : |
Download NASA SP. Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 740 |
Release | : 1975 |
Genre | : Aeronautics |
ISBN | : |
Download NASA SP. Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 636 |
Release | : 1973 |
Genre | : Mechanics, Applied |
ISBN | : |
Download Applied Mechanics Reviews Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 836 |
Release | : 1987 |
Genre | : Heat |
ISBN | : |
Download AIAA 87-1466 - AIAA 87-1538 Book in PDF, Epub and Kindle