Add to ORKGThe drag of a body alone, six triangular wings of various aspect ratios, and the combinations were measured at Mach numbers of 1.50 and 2.02 at a Reynolds number of 5.5 million (based on the body length). The experimental drag-interference results were in accordance with calculations based on NACA RM A9E19, 1949, with skin-friction effects taken into account, the interference effect being principally the result of fixing transition on the body by adding a wing
The lift and pitching-moment characteristics of a body alone, six triangular wings of various aspect...
Drag measurements at transonic speeds on rectangular airfoils and on airfoils swept back 450 are rep...
In a joint effort ONERA and DLR have assessed the interference effects of a generic twin-engine tran...
The drag of a body alone, six triangular wings of various aspect ratios, and the combinations were m...
In order to investigate the effects of drag interference on wing-body combinations, tests were condu...
An investigation of the interference associated with tail surfaces added to wing-fuselage combinatio...
An investigation of the interference associated with tail surfaces added to wing-fuselage combinatio...
This report gives the results of an investigation of the mutual interference of an airfoil and a fla...
Results of an investigation by the free-fall method are presented herein for a configuration having ...
Report presenting an experimental investigation concerned primarily with the extension of test data ...
This report contains the results of an experimental investigation to determine the effects of suppor...
The theory (wing experiments in an artificial air stream are subject to error, due to the fact that ...
The lift and pitching-moment characteristics of a body alone, six triangular wings of various aspect...
Drag measurements at transonic speeds on rectangular airfoils and on airfoils swept back 450 are rep...
In a joint effort ONERA and DLR have assessed the interference effects of a generic twin-engine tran...
The drag of a body alone, six triangular wings of various aspect ratios, and the combinations were m...
In order to investigate the effects of drag interference on wing-body combinations, tests were condu...
An investigation of the interference associated with tail surfaces added to wing-fuselage combinatio...
An investigation of the interference associated with tail surfaces added to wing-fuselage combinatio...
This report gives the results of an investigation of the mutual interference of an airfoil and a fla...
Results of an investigation by the free-fall method are presented herein for a configuration having ...
Report presenting an experimental investigation concerned primarily with the extension of test data ...
This report contains the results of an experimental investigation to determine the effects of suppor...
The theory (wing experiments in an artificial air stream are subject to error, due to the fact that ...
The lift and pitching-moment characteristics of a body alone, six triangular wings of various aspect...
Drag measurements at transonic speeds on rectangular airfoils and on airfoils swept back 450 are rep...
In a joint effort ONERA and DLR have assessed the interference effects of a generic twin-engine tran...