Add to ORKGTransonic similarity rules are applied to the correlation of experimental data for a series of related rectangular wings of varying aspect ratio, thickness, and camber. The data correlation is presented in two parts: the first part presents the correlation for a series of 22 wings having symmetrical NACA 63a-series sections; the second part is concerned with a study of one type of camber by correlation of the data for a series of 18 cambered wings having NACA 63a2xx and 63a4xx sections
This investigation has a double object: 1) the calculation of the general characteristics of certain...
Report presents results of wind tunnel tests of cambered aerofoils and body-wing combinations used f...
This note is the fifth of a series covering an investigation of a number of related airfoils. It pre...
The transonic similarity rules have been applied to the correlation of experimental data for a serie...
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...
The effects of one type of camber on the aerodynamic characteristics of rectangular wings at high su...
Abstract: Some insight into the range of applicability of the transonic area rule has been gained by...
suMMARY Some insight into the range of applicability of the transonic area rule has been gained by’c...
A two-dimensional wind-tunnel investigation of the flow and force characteristics of four NACA 6A-se...
Methodical experiments with the series of airfoil sections of the same relative thickness and of var...
An investigation has been made by the NACA wing-flow method to provide information on the relative l...
This note is one of a series covering an investigation of a number of related airfoils. It presents ...
This note is one of a series covering an investigation of a family of related airfoils. It gives in ...
Report presents the results of an investigation conducted to determine some of the effects of airfoi...
This investigation has a double object: 1) the calculation of the general characteristics of certain...
Report presents results of wind tunnel tests of cambered aerofoils and body-wing combinations used f...
This note is the fifth of a series covering an investigation of a number of related airfoils. It pre...
The transonic similarity rules have been applied to the correlation of experimental data for a serie...
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...
The effects of one type of camber on the aerodynamic characteristics of rectangular wings at high su...
Abstract: Some insight into the range of applicability of the transonic area rule has been gained by...
suMMARY Some insight into the range of applicability of the transonic area rule has been gained by’c...
A two-dimensional wind-tunnel investigation of the flow and force characteristics of four NACA 6A-se...
Methodical experiments with the series of airfoil sections of the same relative thickness and of var...
An investigation has been made by the NACA wing-flow method to provide information on the relative l...
This note is one of a series covering an investigation of a number of related airfoils. It presents ...
This note is one of a series covering an investigation of a family of related airfoils. It gives in ...
Report presents the results of an investigation conducted to determine some of the effects of airfoi...
This investigation has a double object: 1) the calculation of the general characteristics of certain...
Report presents results of wind tunnel tests of cambered aerofoils and body-wing combinations used f...
This note is the fifth of a series covering an investigation of a number of related airfoils. It pre...