Add to ORKGPressure and spanwise load distributions on a first-generation jet transport semispan model at high subsonic speeds are presented for the basic wing and for configurations with an upper winglet only, upper and lower winglets, and a simple wing-tip extension. Selected data are discussed to show the general trends and effects of the various configurations
The effects of winglets on the static aerodynamic stability characteristics of a KC-135A jet transpo...
A baseline wing and a version of the same wing fitted with winglets were tested. The longitudinal ae...
Some experimental flutter results are presented over a Mach number range from about 0.70 to 0.95 for...
Pressure and spanwise load distributions on a first-generation jet transport semispan model at a Mac...
Pressure and spanwise load distributions on a first-generation jet transport semispan model at subso...
The effects of winglets and a simple wing-tip extension on the aerodynamic forces and moments and th...
The effect of sideslip on winglet loads and selected wing loads was investigated at high and low sub...
The effects of winglets on the aerodynamic forces and moments, loads, and crossflow velocities behin...
"The effect of sideslip on winglet loads and selected wing loads was investigated at high and low su...
Winglets, which are small, nearly vertical, winglike surfaces, substantially reduce drag coefficient...
Results of wind tunnel investigations of four jet transport configurations representing both narrow ...
The results of wind tunnel investigations of winglets on four jet transport configurations are prese...
The static longitudinal and lateral directional characteristics of a 0.035 scale model of a first ge...
The static longitudinal and lateral directional characteristics of a 0.035 scale model of a first ge...
A wind tunnel investigation was conducted on a generic, high-wing transport model in the Langley 14-...
The effects of winglets on the static aerodynamic stability characteristics of a KC-135A jet transpo...
A baseline wing and a version of the same wing fitted with winglets were tested. The longitudinal ae...
Some experimental flutter results are presented over a Mach number range from about 0.70 to 0.95 for...
Pressure and spanwise load distributions on a first-generation jet transport semispan model at a Mac...
Pressure and spanwise load distributions on a first-generation jet transport semispan model at subso...
The effects of winglets and a simple wing-tip extension on the aerodynamic forces and moments and th...
The effect of sideslip on winglet loads and selected wing loads was investigated at high and low sub...
The effects of winglets on the aerodynamic forces and moments, loads, and crossflow velocities behin...
"The effect of sideslip on winglet loads and selected wing loads was investigated at high and low su...
Winglets, which are small, nearly vertical, winglike surfaces, substantially reduce drag coefficient...
Results of wind tunnel investigations of four jet transport configurations representing both narrow ...
The results of wind tunnel investigations of winglets on four jet transport configurations are prese...
The static longitudinal and lateral directional characteristics of a 0.035 scale model of a first ge...
The static longitudinal and lateral directional characteristics of a 0.035 scale model of a first ge...
A wind tunnel investigation was conducted on a generic, high-wing transport model in the Langley 14-...
The effects of winglets on the static aerodynamic stability characteristics of a KC-135A jet transpo...
A baseline wing and a version of the same wing fitted with winglets were tested. The longitudinal ae...
Some experimental flutter results are presented over a Mach number range from about 0.70 to 0.95 for...