Add to ORKGLarge scale wind tunnel tests to improve longitudinal stability of supersonic transports with variable swept wing
Low speed static and dynamic longitudinal, and lateral stability of scale model of supersonic transp...
Tests have been conducted in the Langley full-scale tunnel to determine the aerodynamic characterist...
Static longitudinal and lateral aerodynamic characteristics of V/STOL aircraft with variable sweep w...
Large scale wind tunnel investigation of low speed aerodynamic characteristics of supersonic transpo...
Wind tunnel tests to determine low speed high lift aerodynamics of one-fifth scale variable sweep su...
Tests were conducted in the Langley full-scale tunnel to determine the aerodynamic characteristics a...
Low speed wind tunnel testing of high aspect ratio variable sweep wing supersonic transport model fo...
Static longitudinal stability and control at angles of attack above those for wing stall in large-sc...
Wind tunnel studies at supersonic and transonic speeds to determine aerodynamic characteristics of v...
High lift characteristics of variable-sweep transport model with blended engine-fuselage and engine-...
Stability and control of variable sweep wing configuration with outboard wing panels swept back 75 d...
Wind tunnel testing to determine effects of wing planform modifications on longitudinal aerodynamic ...
A low-speed investigation was made on a highly-swept arrow-wing model to determine the effect of win...
Aerodynamic characteristics of aircraft configuration for low level supersonic attack tested in tran...
Wind tunnel tests of stability and control of variable sweep wing aircraft at Mach 1.9
Low speed static and dynamic longitudinal, and lateral stability of scale model of supersonic transp...
Tests have been conducted in the Langley full-scale tunnel to determine the aerodynamic characterist...
Static longitudinal and lateral aerodynamic characteristics of V/STOL aircraft with variable sweep w...
Large scale wind tunnel investigation of low speed aerodynamic characteristics of supersonic transpo...
Wind tunnel tests to determine low speed high lift aerodynamics of one-fifth scale variable sweep su...
Tests were conducted in the Langley full-scale tunnel to determine the aerodynamic characteristics a...
Low speed wind tunnel testing of high aspect ratio variable sweep wing supersonic transport model fo...
Static longitudinal stability and control at angles of attack above those for wing stall in large-sc...
Wind tunnel studies at supersonic and transonic speeds to determine aerodynamic characteristics of v...
High lift characteristics of variable-sweep transport model with blended engine-fuselage and engine-...
Stability and control of variable sweep wing configuration with outboard wing panels swept back 75 d...
Wind tunnel testing to determine effects of wing planform modifications on longitudinal aerodynamic ...
A low-speed investigation was made on a highly-swept arrow-wing model to determine the effect of win...
Aerodynamic characteristics of aircraft configuration for low level supersonic attack tested in tran...
Wind tunnel tests of stability and control of variable sweep wing aircraft at Mach 1.9
Low speed static and dynamic longitudinal, and lateral stability of scale model of supersonic transp...
Tests have been conducted in the Langley full-scale tunnel to determine the aerodynamic characterist...
Static longitudinal and lateral aerodynamic characteristics of V/STOL aircraft with variable sweep w...