Add to ORKGThe effects of one type of camber on the aerodynamic characteristics of rectangular wings at high subsonic and transonic speeds have been studied by applying the transonic similarity rules to the correlation of experimental data for a series of 18 cambered wings having NACA 63A2XX and 63A4XX sections, aspect ratios from 1 to 4, and thicknesses from 4 to 8 percent. The data were obtained by use of a transonic bump over a Mach number range of 0.6 to 1.1
An investigation of the flutter characteristics of a series of thin cantilever wings having taper ra...
An investigation has been made of the effects of conical wing camber and body indentation according ...
An investigation by the transonic-bump technique of the static longitudinal aerodynamic characterist...
Transonic similarity rules are applied to the correlation of experimental data for a series of relat...
The effects of one type of camber on the aerodynamic characteristics of rectangular wings at high su...
Transonic similarity rules are applied to the correlation of experimental data for a series of relat...
The transonic similarity rules have been applied to the correlation of experimental data for a serie...
An investigation of two semispan wings swept back 50 degrees 38 minutes was conducted in the Langley...
Effects of conical camber for triangular wing- body-tail combinations on aerodynamic characteristic
An investigation has been made at Mach numbers of 1.61 and 2.01 to determine the aerodynamic charact...
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
An investigation by the transonic-bump technique of the static longitudinal aerodynamic characterist...
An investigation has been made of the effects of conical wing camber and body indentation according ...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
This investigation is a continuation of the experimental and theoretical evaluation of blended wing-...
An investigation of the flutter characteristics of a series of thin cantilever wings having taper ra...
An investigation has been made of the effects of conical wing camber and body indentation according ...
An investigation by the transonic-bump technique of the static longitudinal aerodynamic characterist...
Transonic similarity rules are applied to the correlation of experimental data for a series of relat...
The effects of one type of camber on the aerodynamic characteristics of rectangular wings at high su...
Transonic similarity rules are applied to the correlation of experimental data for a series of relat...
The transonic similarity rules have been applied to the correlation of experimental data for a serie...
An investigation of two semispan wings swept back 50 degrees 38 minutes was conducted in the Langley...
Effects of conical camber for triangular wing- body-tail combinations on aerodynamic characteristic
An investigation has been made at Mach numbers of 1.61 and 2.01 to determine the aerodynamic charact...
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
An investigation by the transonic-bump technique of the static longitudinal aerodynamic characterist...
An investigation has been made of the effects of conical wing camber and body indentation according ...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
This investigation is a continuation of the experimental and theoretical evaluation of blended wing-...
An investigation of the flutter characteristics of a series of thin cantilever wings having taper ra...
An investigation has been made of the effects of conical wing camber and body indentation according ...
An investigation by the transonic-bump technique of the static longitudinal aerodynamic characterist...