Add to ORKGThe Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determine the longitudinal and lateral-directional aerodynamic characteristics of a winged single-state-to-orbit vehicle was investigated. The model was tested over a Mach number range from 0.3 to 4.63 for an angle-of-attack range from 4 to 30 D at both 0 and 5 D sideslip
A modified triangular wing of aspect ratio 2.53 having an airfoil section 3.7 percent thick at the r...
Hypersonic stability, control, and performance characteristics were determined on a single-stage-to-...
The static aerodynamic characteristics of a 1/30 scale model of a wing-body concept for a high speed...
Transonic pressure and wind tunnel studies were performed to determine the longitudinal and lateral ...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
Experimental aerodynamic characteristics were obtained for a generic, winged, circular-body, single-...
The model was a full-scale mockup of a light single-engine high-wing monoplane. Tests were made over...
An investigation was made in the Langley Unitary Plan wind tunnel at Mach numbers of 2.30, 2.96, and...
Tests were performed in the Langley Unitary Plan wind tunnel to determine the drag and static longit...
Horizontal-tail height, wing height, and dihedral effects on longitudinal and lateral stability char...
An investigation has been conducted in the Langley Unitary Plan wind tunnel to determine the static ...
An experimental investigation of the static longitudinal and lateral-directional aerodynamic charact...
Wind-tunnel studies have been performed in the Langley Hypersonic Helium Tunnel Facility to obtain s...
Results of an investigation of the static longitudinal stability and control characteristics of an a...
An investigation has been conducted at Mach numbers from 2.30 to 4.63 to determine the static aerody...
A modified triangular wing of aspect ratio 2.53 having an airfoil section 3.7 percent thick at the r...
Hypersonic stability, control, and performance characteristics were determined on a single-stage-to-...
The static aerodynamic characteristics of a 1/30 scale model of a wing-body concept for a high speed...
Transonic pressure and wind tunnel studies were performed to determine the longitudinal and lateral ...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
Experimental aerodynamic characteristics were obtained for a generic, winged, circular-body, single-...
The model was a full-scale mockup of a light single-engine high-wing monoplane. Tests were made over...
An investigation was made in the Langley Unitary Plan wind tunnel at Mach numbers of 2.30, 2.96, and...
Tests were performed in the Langley Unitary Plan wind tunnel to determine the drag and static longit...
Horizontal-tail height, wing height, and dihedral effects on longitudinal and lateral stability char...
An investigation has been conducted in the Langley Unitary Plan wind tunnel to determine the static ...
An experimental investigation of the static longitudinal and lateral-directional aerodynamic charact...
Wind-tunnel studies have been performed in the Langley Hypersonic Helium Tunnel Facility to obtain s...
Results of an investigation of the static longitudinal stability and control characteristics of an a...
An investigation has been conducted at Mach numbers from 2.30 to 4.63 to determine the static aerody...
A modified triangular wing of aspect ratio 2.53 having an airfoil section 3.7 percent thick at the r...
Hypersonic stability, control, and performance characteristics were determined on a single-stage-to-...
The static aerodynamic characteristics of a 1/30 scale model of a wing-body concept for a high speed...