Add to ORKGThe influence of ablation on the aerodynamic characteristics of a blunted slender cone was investigated. Plastic models were launched in free flight at ablating conditions. The results were compared with results of similar tests using metal nonablating models. Ablation was found to decrease the dynamic stability and the drag, but had little effect on static stability and lift. The plastic models appeared to experience ablation-induced roll
The emerging and competitive environment in the space technology requires the improvements in the ca...
The drag of spherically blunted conical models of fineness ratio 3 was investigated at Mach numbers ...
A wind-tunnel investigation was conducted at Mach numbers of 2.30 and 4.63 to determine the static a...
A 1000-ft aeroballistics range was used to obtain free-flight stability and drag data for slightly b...
A comprehensive wind tunnel investigation was conducted at Mach number 10 on 4- and 5-deg half-angle...
An experimental investigation of the aerodynamics of a slender cone-cylinder body of revolution was ...
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...
Aerodynamic characteristics of large angle blunt cone with and without fence-type afterbodie
Five spherically blunted cones were tested in free flight, in still air, to determine their aerodyna...
Effect of nose bluntness, fineness ratio, cone angle, and model base on aerodynamic characteristics ...
Axial force, normal force, and pitching moment coefficients of ablating conical Teflon models at Mac...
Static and dynamic stability and drag of blunted and pointed cones at various Mach numbers and Reyno...
Effect of changes in base contour on damping in pitch of blunted cone in wind tunne
Transonic wind tunnel study of aerodynamic characteristics of blunt reentry vehicles at varying angl...
Pressure, force, and dynamic stability tests on spherically blunted cones, and comparison with calcu...
The emerging and competitive environment in the space technology requires the improvements in the ca...
The drag of spherically blunted conical models of fineness ratio 3 was investigated at Mach numbers ...
A wind-tunnel investigation was conducted at Mach numbers of 2.30 and 4.63 to determine the static a...
A 1000-ft aeroballistics range was used to obtain free-flight stability and drag data for slightly b...
A comprehensive wind tunnel investigation was conducted at Mach number 10 on 4- and 5-deg half-angle...
An experimental investigation of the aerodynamics of a slender cone-cylinder body of revolution was ...
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...
Aerodynamic characteristics of large angle blunt cone with and without fence-type afterbodie
Five spherically blunted cones were tested in free flight, in still air, to determine their aerodyna...
Effect of nose bluntness, fineness ratio, cone angle, and model base on aerodynamic characteristics ...
Axial force, normal force, and pitching moment coefficients of ablating conical Teflon models at Mac...
Static and dynamic stability and drag of blunted and pointed cones at various Mach numbers and Reyno...
Effect of changes in base contour on damping in pitch of blunted cone in wind tunne
Transonic wind tunnel study of aerodynamic characteristics of blunt reentry vehicles at varying angl...
Pressure, force, and dynamic stability tests on spherically blunted cones, and comparison with calcu...
The emerging and competitive environment in the space technology requires the improvements in the ca...
The drag of spherically blunted conical models of fineness ratio 3 was investigated at Mach numbers ...
A wind-tunnel investigation was conducted at Mach numbers of 2.30 and 4.63 to determine the static a...