Simplified theoretical approaches are shown, based on hypersonic similarity boundary-layer theory, which allow reasonably accurate estimates to be made of the surface pressures on plates on which viscous effects are important. The consideration of viscous effects includes the cases where curved surfaces, stream pressure gradients, and leadingedge bluntness are important factors
The theory of Taylor and Maccoll (Ref,1) gives the surface pressure on an infinite cone in supersoni...
Hypersonic airbreathing propulsion has been under research since the mid 1960s and will continue to...
For the three dimensional hypersonic viscous compressible flat plate flow, when there is only small ...
A procedure based on the method of similar solutions is presented by which the skin friction, heat t...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77561/1/AIAA-8284-795.pd
Leading edge effects on laminar flat plate boundary layer and aerodynamic heating at Mach 10.
Integral methods in compressible laminar boundary layers applied to self-induced hypersonic pressure...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
The properties of incompressible, unsteady, interactive, boundary layers are examined for a model hy...
Pressure, heat transfer, and skin friction studies on sharp and blunt flat plates at hypersonic spee...
The present study was suggested by several problems and difficulties that had appeared in previous e...
Using the model developed by the author for zero-pressure gradient turbulent boundary layers, result...
Approximate methods for calculating the surface pressures including the effects of viscous interacti...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1961.In...
An asymptotic description is derived for the interaction between a shock wave and a turbulent bounda...
The theory of Taylor and Maccoll (Ref,1) gives the surface pressure on an infinite cone in supersoni...
Hypersonic airbreathing propulsion has been under research since the mid 1960s and will continue to...
For the three dimensional hypersonic viscous compressible flat plate flow, when there is only small ...
A procedure based on the method of similar solutions is presented by which the skin friction, heat t...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77561/1/AIAA-8284-795.pd
Leading edge effects on laminar flat plate boundary layer and aerodynamic heating at Mach 10.
Integral methods in compressible laminar boundary layers applied to self-induced hypersonic pressure...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
The properties of incompressible, unsteady, interactive, boundary layers are examined for a model hy...
Pressure, heat transfer, and skin friction studies on sharp and blunt flat plates at hypersonic spee...
The present study was suggested by several problems and difficulties that had appeared in previous e...
Using the model developed by the author for zero-pressure gradient turbulent boundary layers, result...
Approximate methods for calculating the surface pressures including the effects of viscous interacti...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1961.In...
An asymptotic description is derived for the interaction between a shock wave and a turbulent bounda...
The theory of Taylor and Maccoll (Ref,1) gives the surface pressure on an infinite cone in supersoni...
Hypersonic airbreathing propulsion has been under research since the mid 1960s and will continue to...
For the three dimensional hypersonic viscous compressible flat plate flow, when there is only small ...