Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77561/1/AIAA-8284-795.pd
The paper aimed at studying the peculiarities of boundary layer on a rotating body. Rotation of axis...
The M*ɪ.0 hypersonic, laminar, axisymmetric mean flows past blunt, circular cones at zero angle ...
A numerical study was conducted to investigate the effects of blunt leading edges on the viscous flo...
Simplified theoretical approaches are shown, based on hypersonic similarity boundary-layer theory, w...
Hypersonic flows over cones and straight biconic configurations are calculated for a wide range of f...
An experimental investigation of the aerodynamics of a slender cone-cylinder body of revolution was ...
The theory of Taylor and Maccoll (Ref,1) gives the surface pressure on an infinite cone in supersoni...
A numerical study has been conducted to investigate the effects of blunt leading edges on the viscou...
Pressure distribution and flow fields of blunted cones at hypersonic Mach number
An experimental investigation of viscous effects on static and impact pressure probes was conducted ...
The jet control effectiveness of a 5 deg semi-angle cone has been tested at hypersonic speeds. The ...
In hypersonic flow over slender bodies an important concern is the influence of nose bluntness on th...
The three-dimensional leeward separation about a 5-deg semi-angle cone of 11 deg angle of incidence ...
The aim of present study is to obtain mathematical expressions for surface pressure and its derivati...
A comprehensive wind tunnel investigation was conducted at Mach number 10 on 4- and 5-deg half-angle...
The paper aimed at studying the peculiarities of boundary layer on a rotating body. Rotation of axis...
The M*ɪ.0 hypersonic, laminar, axisymmetric mean flows past blunt, circular cones at zero angle ...
A numerical study was conducted to investigate the effects of blunt leading edges on the viscous flo...
Simplified theoretical approaches are shown, based on hypersonic similarity boundary-layer theory, w...
Hypersonic flows over cones and straight biconic configurations are calculated for a wide range of f...
An experimental investigation of the aerodynamics of a slender cone-cylinder body of revolution was ...
The theory of Taylor and Maccoll (Ref,1) gives the surface pressure on an infinite cone in supersoni...
A numerical study has been conducted to investigate the effects of blunt leading edges on the viscou...
Pressure distribution and flow fields of blunted cones at hypersonic Mach number
An experimental investigation of viscous effects on static and impact pressure probes was conducted ...
The jet control effectiveness of a 5 deg semi-angle cone has been tested at hypersonic speeds. The ...
In hypersonic flow over slender bodies an important concern is the influence of nose bluntness on th...
The three-dimensional leeward separation about a 5-deg semi-angle cone of 11 deg angle of incidence ...
The aim of present study is to obtain mathematical expressions for surface pressure and its derivati...
A comprehensive wind tunnel investigation was conducted at Mach number 10 on 4- and 5-deg half-angle...
The paper aimed at studying the peculiarities of boundary layer on a rotating body. Rotation of axis...
The M*ɪ.0 hypersonic, laminar, axisymmetric mean flows past blunt, circular cones at zero angle ...
A numerical study was conducted to investigate the effects of blunt leading edges on the viscous flo...
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