Add to ORKGPlanform effects on low speed aerodynamic characteristics of triangular and modified triangular wing
A flight investigation of rocket-powered models of a tailless triangular-wing airplane configuration...
An investigation has been conducted at low subsonic speeds to study the effects of canard planform a...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
A low-speed investigation was made in the 6- by 6-foot curved-flow test section of the Langley stabi...
Theoretical and experimental data for wing-body combinations with wings of triangular, arrow, and di...
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
Methods based on the linearized theory for supersonic flow were used to find the characteristics of ...
Data obtained from wind tunnel investigations of two series of 11 triangular wings conducted at Mach...
The lift, drag, and pitching-moment characteristics of a triangular wing, having an aspect ratio of ...
A set of empirical methods was developed to predict low-speed lift, drag and pitching-moment variati...
The purpose of this report is to expand knowledge on the lift and drag properties of thin triangular...
The analysis of the stability derivatives of low-aspect-ratio triangular wings at subsonic and super...
A modified triangular wing of aspect ratio 2.53 having an airfoil section 3.7 percent thick at the r...
Aerodynamic characteristics of triangular planform wing models at supersonic speed
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...
An investigation has been conducted at low subsonic speeds to study the effects of canard planform a...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
A low-speed investigation was made in the 6- by 6-foot curved-flow test section of the Langley stabi...
Theoretical and experimental data for wing-body combinations with wings of triangular, arrow, and di...
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
Methods based on the linearized theory for supersonic flow were used to find the characteristics of ...
Data obtained from wind tunnel investigations of two series of 11 triangular wings conducted at Mach...
The lift, drag, and pitching-moment characteristics of a triangular wing, having an aspect ratio of ...
A set of empirical methods was developed to predict low-speed lift, drag and pitching-moment variati...
The purpose of this report is to expand knowledge on the lift and drag properties of thin triangular...
The analysis of the stability derivatives of low-aspect-ratio triangular wings at subsonic and super...
A modified triangular wing of aspect ratio 2.53 having an airfoil section 3.7 percent thick at the r...
Aerodynamic characteristics of triangular planform wing models at supersonic speed
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...
An investigation has been conducted at low subsonic speeds to study the effects of canard planform a...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration