Add to ORKGStability and control of supersonic vtol airplane model having broad fuselage and small delta win
Flight test to determine flying qualities and dynamic stability derivatives of supersonic fighter ai...
Low speed static and dynamic longitudinal, and lateral stability of scale model of supersonic transp...
The Bell D-188A VTOL airplane is a horizontal-attitude VTOL fighter with tilting engine nacelles at ...
Static stability and control characteristics of aircraft model with tail surfaces outboard of wing t...
An investigation has been conducted at the Langley 4- by 4-foot supersonic pressure tunnel at a Mach...
Dynamic stability and control characteristics of 0.18 scale model of fan-in-wing VTOL aircraf
Flight-determined stability & control derivatives of supersonic aircraft with low aspect ratio unswe...
Stability and control of variable sweep wing configuration with outboard wing panels swept back 75 d...
Effects of wing vertical location on stability and control of canard aircraft at supersonic speed
Longitudinal and lateral stability characteristics of two four-jet VTOL models in transition speed r...
An investigation was made of the static longitudinal stability, and control and stall characteristic...
Wing height effect on stability and control of 70 deg delta-wing canard-aircraft configuration at Ma...
Longitudinal aerodynamic characteristics at transonic speeds of V/STOL aircraft configuration with f...
A TF-8A airplane was equipped with a transport type supercritical wing and fuselage fairings to eval...
Flight investigation of the longitudinal stability and control characteristics of a four-propeller t...
Flight test to determine flying qualities and dynamic stability derivatives of supersonic fighter ai...
Low speed static and dynamic longitudinal, and lateral stability of scale model of supersonic transp...
The Bell D-188A VTOL airplane is a horizontal-attitude VTOL fighter with tilting engine nacelles at ...
Static stability and control characteristics of aircraft model with tail surfaces outboard of wing t...
An investigation has been conducted at the Langley 4- by 4-foot supersonic pressure tunnel at a Mach...
Dynamic stability and control characteristics of 0.18 scale model of fan-in-wing VTOL aircraf
Flight-determined stability & control derivatives of supersonic aircraft with low aspect ratio unswe...
Stability and control of variable sweep wing configuration with outboard wing panels swept back 75 d...
Effects of wing vertical location on stability and control of canard aircraft at supersonic speed
Longitudinal and lateral stability characteristics of two four-jet VTOL models in transition speed r...
An investigation was made of the static longitudinal stability, and control and stall characteristic...
Wing height effect on stability and control of 70 deg delta-wing canard-aircraft configuration at Ma...
Longitudinal aerodynamic characteristics at transonic speeds of V/STOL aircraft configuration with f...
A TF-8A airplane was equipped with a transport type supercritical wing and fuselage fairings to eval...
Flight investigation of the longitudinal stability and control characteristics of a four-propeller t...
Flight test to determine flying qualities and dynamic stability derivatives of supersonic fighter ai...
Low speed static and dynamic longitudinal, and lateral stability of scale model of supersonic transp...
The Bell D-188A VTOL airplane is a horizontal-attitude VTOL fighter with tilting engine nacelles at ...