Leading edge bluntness and ramp deflection angle effects on laminar boundary layer separation in hypersonic flo
Large downstream movements of transition observed when the leading edge of a hollow cylinder or a fl...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
none5The flow field around sharp leading edges in subsonic, low Reynolds number flow is investigated...
An investigation to determine the effects of leading-edge bluntness on the characteristics of lamina...
Prepared at Langley Research Center."February 1966"--Cover.Includes bibliographical references (p. 2...
Low density, leading edge bluntness, and ablation effects on wedge induced laminar boundary layer se...
Shock Boundary Layer Interactions (SBLIs) and shock-shock interactions are some of the most fundamen...
Leading edge effects on laminar flat plate boundary layer and aerodynamic heating at Mach 10.
A numerical and analytical investigation of hypersonic leading edge separation has been conducted. T...
Laminar flow separation on flat plate induced by deflected trailing-edge flap at hypersonic spee
The effects of wall cooling and nose bluntness on laminar and transitional reattaching flows induced...
A change in flow pattern that was observed as the free-stream Mach number was increased in the vicin...
p 1 / S 6 0 An investigation has been made i n the Langley l5-inch hypersonic flow apparatus t o es ...
The effects of leading-edge bluntness and sweep on boundary-layer transition on flat plate models we...
AbstractThe leading edge bluntness effects on inlet boundary layer transition had been studied based...
Large downstream movements of transition observed when the leading edge of a hollow cylinder or a fl...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
none5The flow field around sharp leading edges in subsonic, low Reynolds number flow is investigated...
An investigation to determine the effects of leading-edge bluntness on the characteristics of lamina...
Prepared at Langley Research Center."February 1966"--Cover.Includes bibliographical references (p. 2...
Low density, leading edge bluntness, and ablation effects on wedge induced laminar boundary layer se...
Shock Boundary Layer Interactions (SBLIs) and shock-shock interactions are some of the most fundamen...
Leading edge effects on laminar flat plate boundary layer and aerodynamic heating at Mach 10.
A numerical and analytical investigation of hypersonic leading edge separation has been conducted. T...
Laminar flow separation on flat plate induced by deflected trailing-edge flap at hypersonic spee
The effects of wall cooling and nose bluntness on laminar and transitional reattaching flows induced...
A change in flow pattern that was observed as the free-stream Mach number was increased in the vicin...
p 1 / S 6 0 An investigation has been made i n the Langley l5-inch hypersonic flow apparatus t o es ...
The effects of leading-edge bluntness and sweep on boundary-layer transition on flat plate models we...
AbstractThe leading edge bluntness effects on inlet boundary layer transition had been studied based...
Large downstream movements of transition observed when the leading edge of a hollow cylinder or a fl...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
none5The flow field around sharp leading edges in subsonic, low Reynolds number flow is investigated...
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