Add to ORKGAn experimental investigation was conducted in an 11- by 11-foot wind tunnel to determine the aerodynamic characteristics of an oblique high aspect ratio wing in combination with a high fineness-ratio Sears-Haack body. Longitudinal and lateral-directional stability data were obtained at wing yaw angles from 0 deg to 60 deg over a test Mach number range from 0.6 to 1.4 for angles of attack between minus 6 deg and 9 deg. The effects of changes in Reynolds number, dihedral, and trailing-edge angle were studied along with the effects of a roughness strip on the upper and lower surfaces of the wing. Flow-visualization studies were made to determine the nature of the flow on the wing surfaces
Results are presented of wind-tunnel investigations at Mach numbers of 0.60 to 0.94 and angles of at...
The experimental longitudinal-and lateral-directional stability characteristics of a Langley concept...
Aerodynamic interference effects were studied for two slender, streamlined bodies of revolution at M...
An experimental investigation was conducted in an 11- by 11-foot transonic wind tunnel to study the ...
Models of three practical oblique-wing transport configurations were tested in the NASA Ames 11 foot...
A preliminary flight experiment was flown to generate a full-scale supersonic data base to aid the a...
Four advanced fighter configurations, which differed in wing planform and airfoil shape, were invest...
The results of pressure-distribution and force tests of four wings at a Mach number of about 6.9 and...
An experimental investigation was conducted in the Ames 14-foot transonic wind tunnel to study the a...
Wind-tunnel tests of a full-scale model of the Republic XP-91 airplane were conducted to determine t...
An experimental investigation was conducted to provide a systematic set of lateral-directional stabi...
Flow-angle and pressure surveys behind five, thin, pointed-tip wings of varying plan form have been ...
The lift, pitching-moment, and drag characteristics of a missile configuration having a body of fine...
The experimental aerodynamic characteristics of three basic wing planforms on a conceptual orbiter f...
This report presents the results of an investigation conducted in the Langley 300 mph 7- by 10-foot ...
Results are presented of wind-tunnel investigations at Mach numbers of 0.60 to 0.94 and angles of at...
The experimental longitudinal-and lateral-directional stability characteristics of a Langley concept...
Aerodynamic interference effects were studied for two slender, streamlined bodies of revolution at M...
An experimental investigation was conducted in an 11- by 11-foot transonic wind tunnel to study the ...
Models of three practical oblique-wing transport configurations were tested in the NASA Ames 11 foot...
A preliminary flight experiment was flown to generate a full-scale supersonic data base to aid the a...
Four advanced fighter configurations, which differed in wing planform and airfoil shape, were invest...
The results of pressure-distribution and force tests of four wings at a Mach number of about 6.9 and...
An experimental investigation was conducted in the Ames 14-foot transonic wind tunnel to study the a...
Wind-tunnel tests of a full-scale model of the Republic XP-91 airplane were conducted to determine t...
An experimental investigation was conducted to provide a systematic set of lateral-directional stabi...
Flow-angle and pressure surveys behind five, thin, pointed-tip wings of varying plan form have been ...
The lift, pitching-moment, and drag characteristics of a missile configuration having a body of fine...
The experimental aerodynamic characteristics of three basic wing planforms on a conceptual orbiter f...
This report presents the results of an investigation conducted in the Langley 300 mph 7- by 10-foot ...
Results are presented of wind-tunnel investigations at Mach numbers of 0.60 to 0.94 and angles of at...
The experimental longitudinal-and lateral-directional stability characteristics of a Langley concept...
Aerodynamic interference effects were studied for two slender, streamlined bodies of revolution at M...