Add to ORKGLarge scale wind tunnel investigation of low speed aerodynamic characteristics of supersonic transport model having variable sweep wing
Large scale low speed wind tunnel tests of delta winged supersonic transport model to determine aero...
Stability and control of variable sweep wing configuration with outboard wing panels swept back 75 d...
Wind tunnel tests of stability and control of variable sweep wing aircraft at Mach 1.9
Large scale wind tunnel tests to improve longitudinal stability of supersonic transports with variab...
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...
Wind tunnel studies at supersonic and transonic speeds to determine aerodynamic characteristics of v...
Transonic aerodynamic characteristics of two variable sweep aircraft configurations capable of low l...
Low speed wind tunnel testing of high aspect ratio variable sweep wing supersonic transport model fo...
Tests have been conducted in the Langley full-scale tunnel to determine the aerodynamic characterist...
Aerodynamic characteristics of aircraft configuration for low level supersonic attack tested in tran...
Aerodynamic characteristics of variable sweep aircraft configurations - low altitude supersonic vehi...
High lift characteristics of variable-sweep transport model with blended engine-fuselage and engine-...
Low speed static and dynamic longitudinal, and lateral stability of scale model of supersonic transp...
The low-speed characteristics of a large-scale model of the U. S. Navy/Grumman F-14A aircraft were s...
Large scale low speed wind tunnel tests of delta winged supersonic transport model to determine aero...
Stability and control of variable sweep wing configuration with outboard wing panels swept back 75 d...
Wind tunnel tests of stability and control of variable sweep wing aircraft at Mach 1.9
Large scale wind tunnel tests to improve longitudinal stability of supersonic transports with variab...
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...
Wind tunnel studies at supersonic and transonic speeds to determine aerodynamic characteristics of v...
Transonic aerodynamic characteristics of two variable sweep aircraft configurations capable of low l...
Low speed wind tunnel testing of high aspect ratio variable sweep wing supersonic transport model fo...
Tests have been conducted in the Langley full-scale tunnel to determine the aerodynamic characterist...
Aerodynamic characteristics of aircraft configuration for low level supersonic attack tested in tran...
Aerodynamic characteristics of variable sweep aircraft configurations - low altitude supersonic vehi...
High lift characteristics of variable-sweep transport model with blended engine-fuselage and engine-...
Low speed static and dynamic longitudinal, and lateral stability of scale model of supersonic transp...
The low-speed characteristics of a large-scale model of the U. S. Navy/Grumman F-14A aircraft were s...
Large scale low speed wind tunnel tests of delta winged supersonic transport model to determine aero...
Stability and control of variable sweep wing configuration with outboard wing panels swept back 75 d...
Wind tunnel tests of stability and control of variable sweep wing aircraft at Mach 1.9