Add to ORKGA wing-body combination having a plane triangular wing of aspect ratio 2 with NACA 0005-63 thickness distribution in streamwise planes, and twisted and cambered for a trapezoidal span load distribution has been investigated at both subsonic and supersonic Mach numbers. The lift, drag, and pitching moment of the model are presented for Mach numbers from 0.60 to 0.90 and 1.30 to 1.70 at a Reynolds number of 3.0 million. The variations of the characteristics with Reynolds number are also shown for several Mach numbers
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
An investigation of two semispan wings swept back 50 degrees 38 minutes was conducted in the Langley...
The analysis of the stability derivatives of low-aspect-ratio triangular wings at subsonic and super...
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
The lift, drag, and pitching-moment characteristics of a triangular wing, having an aspect ratio of ...
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
This report presents measurements of the lift and pitching-moment characteristics of a straight wing...
An investigation of the characteristics of a wing with an aspect ratio of 9.0 and an NACA 65-210 air...
Theoretical and experimental data for wing-body combinations with wings of triangular, arrow, and di...
Results are presented, in graphical and tabular form, from a wind tunnel investigation of the lift, ...
The results of an experimental investigation of the load distribution over two triangular wings in s...
The results of tests of 22 triangular wings, representing two leading-edge shapes for each of 11 ape...
A modified triangular wing of aspect ratio 2.53 having an airfoil section 3.7 percent thick at the r...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
This paper presents some recently obtained data on the aerodynamic characteristics of low-aspect-rat...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
An investigation of two semispan wings swept back 50 degrees 38 minutes was conducted in the Langley...
The analysis of the stability derivatives of low-aspect-ratio triangular wings at subsonic and super...
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
The lift, drag, and pitching-moment characteristics of a triangular wing, having an aspect ratio of ...
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
This report presents measurements of the lift and pitching-moment characteristics of a straight wing...
An investigation of the characteristics of a wing with an aspect ratio of 9.0 and an NACA 65-210 air...
Theoretical and experimental data for wing-body combinations with wings of triangular, arrow, and di...
Results are presented, in graphical and tabular form, from a wind tunnel investigation of the lift, ...
The results of an experimental investigation of the load distribution over two triangular wings in s...
The results of tests of 22 triangular wings, representing two leading-edge shapes for each of 11 ape...
A modified triangular wing of aspect ratio 2.53 having an airfoil section 3.7 percent thick at the r...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
This paper presents some recently obtained data on the aerodynamic characteristics of low-aspect-rat...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
An investigation of two semispan wings swept back 50 degrees 38 minutes was conducted in the Langley...
The analysis of the stability derivatives of low-aspect-ratio triangular wings at subsonic and super...