Add to ORKGEffect of body nose blunting, control planform area, and leading edge bluntness on aerodynamic control of semivertex cone at hypersonic spee
An experimental investigation has been carried out to study the effect of nose bluntness on the char...
Experimental drag measurements at zero angle of attack for various theoretical minimum drag nose sha...
Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on 5 de...
Effect of nose bluntness, fineness ratio, cone angle, and model base on aerodynamic characteristics ...
Nose bluntness and roughness effect of flow on all-external-compression hypersonic inlet bodie
An investigation has been conducted in the Langley Unitary Plan wind tunnel to determine the effects...
An experimental investigation has been carried out13; to study the effect of nose bluntness on the13...
Effect of changes in base contour on damping in pitch of blunted cone in wind tunne
A cone with a blunt nose tip and a 10.7 deg cone half angle and an ogive with a blunt nose tip and a...
An experimental investigation has been car ked out to study the effect of nose bluntness on the char...
Experimental values of shock shapes (angles of attack of 0 deg and 10 deg) and static aerodynamic co...
Static and dynamic stability and drag of blunted and pointed cones at various Mach numbers and Reyno...
In this report, the effect of nose blunting for side force alleviation are addressed in significant ...
Longitudinal aerodynamic characteristics of blunted cone reentry vehicle configurations at high Mach...
In this report, the effect of nose blunting for side force alleviation are addressed in significant ...
An experimental investigation has been carried out to study the effect of nose bluntness on the char...
Experimental drag measurements at zero angle of attack for various theoretical minimum drag nose sha...
Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on 5 de...
Effect of nose bluntness, fineness ratio, cone angle, and model base on aerodynamic characteristics ...
Nose bluntness and roughness effect of flow on all-external-compression hypersonic inlet bodie
An investigation has been conducted in the Langley Unitary Plan wind tunnel to determine the effects...
An experimental investigation has been carried out13; to study the effect of nose bluntness on the13...
Effect of changes in base contour on damping in pitch of blunted cone in wind tunne
A cone with a blunt nose tip and a 10.7 deg cone half angle and an ogive with a blunt nose tip and a...
An experimental investigation has been car ked out to study the effect of nose bluntness on the char...
Experimental values of shock shapes (angles of attack of 0 deg and 10 deg) and static aerodynamic co...
Static and dynamic stability and drag of blunted and pointed cones at various Mach numbers and Reyno...
In this report, the effect of nose blunting for side force alleviation are addressed in significant ...
Longitudinal aerodynamic characteristics of blunted cone reentry vehicle configurations at high Mach...
In this report, the effect of nose blunting for side force alleviation are addressed in significant ...
An experimental investigation has been carried out to study the effect of nose bluntness on the char...
Experimental drag measurements at zero angle of attack for various theoretical minimum drag nose sha...
Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on 5 de...