Add to ORKGAn investigation has been carried out to obtain aerodynamic stability and control data on a model of a winged reentry vehicle at Mach numbers of 10.8 and 17.8 in helium. The effects of a booster transition section on the static stability were obtained at angles of attack from -5 deg to 15 deg and at angles of sideslip from -5 deg to 10 deg at an angle of attack of 0 deg. Directional control data were also obtained at an angle of attack of 0 deg for sideslip angles from -5 deg to 10 deg. No detailed analysis of the data has been made
Subsonic flight characteristics of flat-top hypersonic-boost glide airplane model with arrowhead win
Static longitudinal aerodynamics of wing and blunt body shapes for use as reentry configurations at ...
Static force and moment tests of a 0.062-scale model of a hypersonic vehicle study concept known as ...
An investigation of the low-subsonic-speed static longitudinal stability and control characteristics...
An investigation has been conducted to determine the longitudinal stability and control characterist...
Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles ...
An investigation of the low-subsonic stability and control characteristics of a model of a hypersoni...
A low-speed investigation has been made to determine the static and oscillatory longitudinal and lat...
The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determ...
An experimental investigation of the low-speed longitudinal, lateral, and directional stability char...
Stability and control characteristics of reentry vehicle configurations at angles of attack up to 90...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
Static stability and control characteristics of manned lenticular reentry configuration at low subso...
Static longitudinal stability characteristics of blunted glider reentry configuratio
Wind-tunnel studies have been performed in the Langley Hypersonic Helium Tunnel Facility to obtain s...
Subsonic flight characteristics of flat-top hypersonic-boost glide airplane model with arrowhead win
Static longitudinal aerodynamics of wing and blunt body shapes for use as reentry configurations at ...
Static force and moment tests of a 0.062-scale model of a hypersonic vehicle study concept known as ...
An investigation of the low-subsonic-speed static longitudinal stability and control characteristics...
An investigation has been conducted to determine the longitudinal stability and control characterist...
Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles ...
An investigation of the low-subsonic stability and control characteristics of a model of a hypersoni...
A low-speed investigation has been made to determine the static and oscillatory longitudinal and lat...
The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determ...
An experimental investigation of the low-speed longitudinal, lateral, and directional stability char...
Stability and control characteristics of reentry vehicle configurations at angles of attack up to 90...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
Static stability and control characteristics of manned lenticular reentry configuration at low subso...
Static longitudinal stability characteristics of blunted glider reentry configuratio
Wind-tunnel studies have been performed in the Langley Hypersonic Helium Tunnel Facility to obtain s...
Subsonic flight characteristics of flat-top hypersonic-boost glide airplane model with arrowhead win
Static longitudinal aerodynamics of wing and blunt body shapes for use as reentry configurations at ...
Static force and moment tests of a 0.062-scale model of a hypersonic vehicle study concept known as ...