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
This report contains the results of an experimental investigation to determine the effects of suppor...
Wind-tunnel force tests of a number of wing-body combinations designed for high lift-drag ratio at a...
Force and moment characteristics, including lift-drag ratios, have been measured for bodies of circu...
In order to investigate the effects of drag interference on wing-body combinations, tests were condu...
The drag of a body alone, six triangular wings of various aspect ratios, and the combinations were m...
The lift and pitching-moment characteristics of a body alone, six triangular wings of various aspect...
Experimental tests have been conducted to determine possible aerodynamic interference effects due to...
Estimating method for lift interference of wing- body combinations at supersonic speed
Results are given of pressure measurements on awing of gross aspect ratio approximately 2/3 mounted...
Detailed interference force-and-pressure data were obtained on a representative supersonic transport...
An investigation was made of the effects of body shape on the drag of a 45 deg sweptback-wing-body c...
Tests of two wing-body combinations have been conducted in the Langley 19-foot pressure tunnel at a ...
Results of an investigation by the free-fall method are presented herein for a configuration having ...
In order to indicate the effects of Reynolds number and other variables on the drag due to lift of d...
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
This report contains the results of an experimental investigation to determine the effects of suppor...
Wind-tunnel force tests of a number of wing-body combinations designed for high lift-drag ratio at a...
Force and moment characteristics, including lift-drag ratios, have been measured for bodies of circu...
In order to investigate the effects of drag interference on wing-body combinations, tests were condu...
The drag of a body alone, six triangular wings of various aspect ratios, and the combinations were m...
The lift and pitching-moment characteristics of a body alone, six triangular wings of various aspect...
Experimental tests have been conducted to determine possible aerodynamic interference effects due to...
Estimating method for lift interference of wing- body combinations at supersonic speed
Results are given of pressure measurements on awing of gross aspect ratio approximately 2/3 mounted...
Detailed interference force-and-pressure data were obtained on a representative supersonic transport...
An investigation was made of the effects of body shape on the drag of a 45 deg sweptback-wing-body c...
Tests of two wing-body combinations have been conducted in the Langley 19-foot pressure tunnel at a ...
Results of an investigation by the free-fall method are presented herein for a configuration having ...
In order to indicate the effects of Reynolds number and other variables on the drag due to lift of d...
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
This report contains the results of an experimental investigation to determine the effects of suppor...
Wind-tunnel force tests of a number of wing-body combinations designed for high lift-drag ratio at a...
Force and moment characteristics, including lift-drag ratios, have been measured for bodies of circu...