Add to ORKGEffect of boundary layer bleed on heat transfer and pressure distributions over wedge-flap surface at hypersonic speed
An experimental aerodynamic heating investigation was conducted to determine effects of hot boundary...
The development of the flow pattern that arises during the interaction of a shock wave with a wedge ...
Leading edge effects on laminar flat plate boundary layer and aerodynamic heating at Mach 10.
Laminar flow separation on flat plate induced by deflected trailing-edge flap at hypersonic spee
The present study analyses the effects of a number of geometric parameters on the performance of a ...
Hypersonic boundary layer separation and flow field interference analysis during Dyna-Soar space gli...
Heat transfer measurements on flat plate with trailing edge flap in hypersonic flo
Heat transfer in regions of laminar, transitional, and turbulent separation on sharp and blunt leadi...
Low density, leading edge bluntness, and ablation effects on wedge induced laminar boundary layer se...
Two types of flow configurations with bleed in two-dimensional hypersonic flows are numerically exam...
A semi-empirical method is developed to estimate drag on wedge-shaped projections in hypersonic flow...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76964/1/AIAA-1991-32-677.pd
A numerical investigation of a generic reentry vehicle flap configuration at hypersonic speed is pre...
A change in flow pattern that was observed as the free-stream Mach number was increased in the vicin...
Real gas wedge-induced laminar separation on cooled blunt flat plate at hypersonic spee
An experimental aerodynamic heating investigation was conducted to determine effects of hot boundary...
The development of the flow pattern that arises during the interaction of a shock wave with a wedge ...
Leading edge effects on laminar flat plate boundary layer and aerodynamic heating at Mach 10.
Laminar flow separation on flat plate induced by deflected trailing-edge flap at hypersonic spee
The present study analyses the effects of a number of geometric parameters on the performance of a ...
Hypersonic boundary layer separation and flow field interference analysis during Dyna-Soar space gli...
Heat transfer measurements on flat plate with trailing edge flap in hypersonic flo
Heat transfer in regions of laminar, transitional, and turbulent separation on sharp and blunt leadi...
Low density, leading edge bluntness, and ablation effects on wedge induced laminar boundary layer se...
Two types of flow configurations with bleed in two-dimensional hypersonic flows are numerically exam...
A semi-empirical method is developed to estimate drag on wedge-shaped projections in hypersonic flow...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76964/1/AIAA-1991-32-677.pd
A numerical investigation of a generic reentry vehicle flap configuration at hypersonic speed is pre...
A change in flow pattern that was observed as the free-stream Mach number was increased in the vicin...
Real gas wedge-induced laminar separation on cooled blunt flat plate at hypersonic spee
An experimental aerodynamic heating investigation was conducted to determine effects of hot boundary...
The development of the flow pattern that arises during the interaction of a shock wave with a wedge ...
Leading edge effects on laminar flat plate boundary layer and aerodynamic heating at Mach 10.