Add to ORKGTransonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
Aerodynamic wind tunnel study of tailless fixed- wing supersonic transport model at transonic spee
Transonic wind tunnel study of aerodynamic characteristics of blunt reentry vehicles at varying angl...
Effect of rearward body strakes on transonic aerodynamic characteristics of unswept-wing fighter air...
The longitudinal aerodynamic characteristics of a wing-body-horizontal-tail configuration designed f...
The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determ...
An investigation by the transonic-bump technique of the static longitudinal aerodynamic characterist...
Static longitudinal aerodynamics of wing and blunt body shapes for use as reentry configurations at ...
Results are presented of tests conducted in the Langley stability tunnel to determine the effects of...
An investigation by the transonic-bump technique of the static longitudinal aerodynamic characterist...
Transonic wind tunnel study of static longitudinal and lateral stability and control characteristics...
A wind-tunnel investigation was made to determine the longitudinal aerodynamic characteristics of a ...
An investigation of the low-subsonic-speed static longitudinal stability and control characteristics...
An experimental investigation of the low-speed longitudinal, lateral, and directional stability char...
An investigation has been made of the effects of conical wing camber and body indentation according ...
Longitudinal aerodynamic characteristics at Mach numbers 0.50 to 1.19 of supersonic transport model ...
Aerodynamic wind tunnel study of tailless fixed- wing supersonic transport model at transonic spee
Transonic wind tunnel study of aerodynamic characteristics of blunt reentry vehicles at varying angl...
Effect of rearward body strakes on transonic aerodynamic characteristics of unswept-wing fighter air...
The longitudinal aerodynamic characteristics of a wing-body-horizontal-tail configuration designed f...
The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determ...
An investigation by the transonic-bump technique of the static longitudinal aerodynamic characterist...
Static longitudinal aerodynamics of wing and blunt body shapes for use as reentry configurations at ...
Results are presented of tests conducted in the Langley stability tunnel to determine the effects of...
An investigation by the transonic-bump technique of the static longitudinal aerodynamic characterist...
Transonic wind tunnel study of static longitudinal and lateral stability and control characteristics...
A wind-tunnel investigation was made to determine the longitudinal aerodynamic characteristics of a ...
An investigation of the low-subsonic-speed static longitudinal stability and control characteristics...
An experimental investigation of the low-speed longitudinal, lateral, and directional stability char...
An investigation has been made of the effects of conical wing camber and body indentation according ...
Longitudinal aerodynamic characteristics at Mach numbers 0.50 to 1.19 of supersonic transport model ...
Aerodynamic wind tunnel study of tailless fixed- wing supersonic transport model at transonic spee
Transonic wind tunnel study of aerodynamic characteristics of blunt reentry vehicles at varying angl...
Effect of rearward body strakes on transonic aerodynamic characteristics of unswept-wing fighter air...