Add to ORKGForce, stability and control characteristics of three axisymmetric low fineness ratio reentry shapes at Mach 6.
Longitudinal aerodynamic characteristics of blunt, lifting reentry vehicle at mach 0.9
Transonic wind tunnel study of aerodynamic characteristics of blunt reentry vehicles at varying angl...
Effect of cross section shape on low speed aero- dynamic characteristics of low-wave drag hyper- son...
Aerodynamic characteristics of modified conical lifting reentry vehicle at hypersonic speed
Free flying 1/3-scale model of a lifting reentry configuration and low subsonic stability and contro...
Hypersonic aerodynamic characteristics of low fineness ratio variable geometry logistics spacecraft ...
Static longitudinal aerodynamics of wing and blunt body shapes for use as reentry configurations at ...
Static stability and control characteristics of manned lenticular reentry configuration at low subso...
Stability and control characteristics of reentry vehicle configurations at angles of attack up to 90...
Longitudinal, lateral, and directional stability and control characteristics of lifting entry vehicl...
An investigation has been conducted to determine the longitudinal stability and control characterist...
Static longitudinal stability and control characteristics of wingless missile configuration at super...
Low subsonic aerodynamic characteristics of medium hypersonic L/D reentry spacecraft configuration w...
Aerodynamic characteristics of a model designed to represent an all body, hypersonic cruise aircraft...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
Longitudinal aerodynamic characteristics of blunt, lifting reentry vehicle at mach 0.9
Transonic wind tunnel study of aerodynamic characteristics of blunt reentry vehicles at varying angl...
Effect of cross section shape on low speed aero- dynamic characteristics of low-wave drag hyper- son...
Aerodynamic characteristics of modified conical lifting reentry vehicle at hypersonic speed
Free flying 1/3-scale model of a lifting reentry configuration and low subsonic stability and contro...
Hypersonic aerodynamic characteristics of low fineness ratio variable geometry logistics spacecraft ...
Static longitudinal aerodynamics of wing and blunt body shapes for use as reentry configurations at ...
Static stability and control characteristics of manned lenticular reentry configuration at low subso...
Stability and control characteristics of reentry vehicle configurations at angles of attack up to 90...
Longitudinal, lateral, and directional stability and control characteristics of lifting entry vehicl...
An investigation has been conducted to determine the longitudinal stability and control characterist...
Static longitudinal stability and control characteristics of wingless missile configuration at super...
Low subsonic aerodynamic characteristics of medium hypersonic L/D reentry spacecraft configuration w...
Aerodynamic characteristics of a model designed to represent an all body, hypersonic cruise aircraft...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
Longitudinal aerodynamic characteristics of blunt, lifting reentry vehicle at mach 0.9
Transonic wind tunnel study of aerodynamic characteristics of blunt reentry vehicles at varying angl...
Effect of cross section shape on low speed aero- dynamic characteristics of low-wave drag hyper- son...