Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76964/1/AIAA-1991-32-677.pd
Experiments at supersonic speeds and at Mach 8 were conducted to determine the conditions which gove...
Effect of boundary layer bleed on heat transfer and pressure distributions over wedge-flap surface a...
Low density, leading edge bluntness, and ablation effects on wedge induced laminar boundary layer se...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76052/1/AIAA-12372-854.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76211/1/AIAA-10846-311.pd
Aerodynamic forces are obtained for laminar flow past a slender wedge at high Mach number and high R...
An inviscid, compressible analysis is given for massive blowing from the porous surface of a wedge o...
An analysis of inviscid, compressible flow over a porous conne or wedge is given where the body is i...
A semi-empirical method is developed to estimate drag on wedge-shaped projections in hypersonic flow...
A possible means of controlling hypervelocity vehicles within the atmosphere is the use of boundary-...
The development of the flow pattern that arises during the interaction of a shock wave with a wedge ...
This report describes a theoretical and experimental investigation of the properties of attached and...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
Shock Boundary Layer Interactions (SBLIs) and shock-shock interactions are some of the most fundamen...
Real gas wedge-induced laminar separation on cooled blunt flat plate at hypersonic spee
Experiments at supersonic speeds and at Mach 8 were conducted to determine the conditions which gove...
Effect of boundary layer bleed on heat transfer and pressure distributions over wedge-flap surface a...
Low density, leading edge bluntness, and ablation effects on wedge induced laminar boundary layer se...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76052/1/AIAA-12372-854.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76211/1/AIAA-10846-311.pd
Aerodynamic forces are obtained for laminar flow past a slender wedge at high Mach number and high R...
An inviscid, compressible analysis is given for massive blowing from the porous surface of a wedge o...
An analysis of inviscid, compressible flow over a porous conne or wedge is given where the body is i...
A semi-empirical method is developed to estimate drag on wedge-shaped projections in hypersonic flow...
A possible means of controlling hypervelocity vehicles within the atmosphere is the use of boundary-...
The development of the flow pattern that arises during the interaction of a shock wave with a wedge ...
This report describes a theoretical and experimental investigation of the properties of attached and...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
Shock Boundary Layer Interactions (SBLIs) and shock-shock interactions are some of the most fundamen...
Real gas wedge-induced laminar separation on cooled blunt flat plate at hypersonic spee
Experiments at supersonic speeds and at Mach 8 were conducted to determine the conditions which gove...
Effect of boundary layer bleed on heat transfer and pressure distributions over wedge-flap surface a...
Low density, leading edge bluntness, and ablation effects on wedge induced laminar boundary layer se...
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