Add to ORKGA flight investigation of rocket-powered models of a tailless triangular-wing airplane configuration was made through the transonic and low supersonic speed range at the Langley Pilotless Aircraft Research Station at Wallops Island, Va. An analysis of the aerodynamic coefficients, stability derivatives, and flying qualities based on the results obtained from the successful flight tests of three models is presented
A modified triangular wing of aspect ratio 2.53 having an airfoil section 3.7 percent thick at the r...
The static longitudinal, lateral, and directional stability characteristics of a hypersonic research...
A low speed investigation was conducted in the Langley V/STOL tunnel to define the static stability ...
A modified triangular wing of aspect ratio 2.53 having an airfoil section 3.7 percent thick at the r...
A flight investigation of rocket-powered models of a tailless triangular-wing airplane configuration...
Aerodynamic wind tunnel study of tailless fixed- wing supersonic transport model at transonic spee
The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determ...
A test technique and data analysis method has been developed for determining the longitudinal aerody...
Free flight test of tailless missile configuration with 45-deg sweptback wing of aspect ratio 4 - st...
Aerodynamic characteristics of scale model of X-15 research aircraft determined in transonic pressur...
Subsonic flight characteristics of flat-top hypersonic-boost glide airplane model with arrowhead win
A summary and analysis have been made of the results of various investigations to determine the aero...
Flight tests have been conducted on rocket-propelled models of an airplane configuration incorporati...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
An experimental investigation of the low-speed longitudinal, lateral, and directional stability char...
A modified triangular wing of aspect ratio 2.53 having an airfoil section 3.7 percent thick at the r...
The static longitudinal, lateral, and directional stability characteristics of a hypersonic research...
A low speed investigation was conducted in the Langley V/STOL tunnel to define the static stability ...
A modified triangular wing of aspect ratio 2.53 having an airfoil section 3.7 percent thick at the r...
A flight investigation of rocket-powered models of a tailless triangular-wing airplane configuration...
Aerodynamic wind tunnel study of tailless fixed- wing supersonic transport model at transonic spee
The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determ...
A test technique and data analysis method has been developed for determining the longitudinal aerody...
Free flight test of tailless missile configuration with 45-deg sweptback wing of aspect ratio 4 - st...
Aerodynamic characteristics of scale model of X-15 research aircraft determined in transonic pressur...
Subsonic flight characteristics of flat-top hypersonic-boost glide airplane model with arrowhead win
A summary and analysis have been made of the results of various investigations to determine the aero...
Flight tests have been conducted on rocket-propelled models of an airplane configuration incorporati...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
An experimental investigation of the low-speed longitudinal, lateral, and directional stability char...
A modified triangular wing of aspect ratio 2.53 having an airfoil section 3.7 percent thick at the r...
The static longitudinal, lateral, and directional stability characteristics of a hypersonic research...
A low speed investigation was conducted in the Langley V/STOL tunnel to define the static stability ...