Add to ORKGLow density, leading edge bluntness, and ablation effects on wedge induced laminar boundary layer separation at moderate enthalpies in hypersonic flo
Prepared at Langley Research Center."February 1966"--Cover.Includes bibliographical references (p. 2...
The influence of leading-edge geometry on boundary-layer transition on a hollow cylinder aligned wit...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76964/1/AIAA-1991-32-677.pd
Real gas wedge-induced laminar separation on cooled blunt flat plate at hypersonic spee
Leading edge bluntness and ramp deflection angle effects on laminar boundary layer separation in hyp...
Hypersonic laminar flow separation preceded by an expansion typically occurs in practical flow situa...
Leading edge effects on laminar flat plate boundary layer and aerodynamic heating at Mach 10.
An investigation to determine the effects of leading-edge bluntness on the characteristics of lamina...
Large downstream movements of transition observed when the leading edge of a hollow cylinder or a fl...
A numerical and analytical investigation of hypersonic leading edge separation has been conducted. T...
Recent results of the effects of Mach number, stream turbulence, leading-edge geometry, leading-edge...
Measuring low-density flow over two-dimensional blunt bodies in hypersonic arc tunne
Abstract. A hypersonic flow about a cylindrically blunted thick plate at a zero angle of attack is n...
Large doumtream nwvementa of tran8i&rn obst%wedwhen the leading edge of a)iOUowqlinder or a jlzt...
Effect of boundary layer bleed on heat transfer and pressure distributions over wedge-flap surface a...
Prepared at Langley Research Center."February 1966"--Cover.Includes bibliographical references (p. 2...
The influence of leading-edge geometry on boundary-layer transition on a hollow cylinder aligned wit...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76964/1/AIAA-1991-32-677.pd
Real gas wedge-induced laminar separation on cooled blunt flat plate at hypersonic spee
Leading edge bluntness and ramp deflection angle effects on laminar boundary layer separation in hyp...
Hypersonic laminar flow separation preceded by an expansion typically occurs in practical flow situa...
Leading edge effects on laminar flat plate boundary layer and aerodynamic heating at Mach 10.
An investigation to determine the effects of leading-edge bluntness on the characteristics of lamina...
Large downstream movements of transition observed when the leading edge of a hollow cylinder or a fl...
A numerical and analytical investigation of hypersonic leading edge separation has been conducted. T...
Recent results of the effects of Mach number, stream turbulence, leading-edge geometry, leading-edge...
Measuring low-density flow over two-dimensional blunt bodies in hypersonic arc tunne
Abstract. A hypersonic flow about a cylindrically blunted thick plate at a zero angle of attack is n...
Large doumtream nwvementa of tran8i&rn obst%wedwhen the leading edge of a)iOUowqlinder or a jlzt...
Effect of boundary layer bleed on heat transfer and pressure distributions over wedge-flap surface a...
Prepared at Langley Research Center."February 1966"--Cover.Includes bibliographical references (p. 2...
The influence of leading-edge geometry on boundary-layer transition on a hollow cylinder aligned wit...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76964/1/AIAA-1991-32-677.pd