Add to ORKGProfile change effects on aerodynamic characteristics of twisted and cambered arrow wing at supersonic spee
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
Effects of airfoil section shape and thickness on supersonic performance characteristics of wing bod...
Engine nacelle orientation effect on aerodynamic characteristics of arrow wing body configuratio
A series of arrow wings employing various degrees of twist and camber were tested in the Langley 4- ...
An investigation has been made at Mach numbers of 1.61 and 2.01 to determine the aerodynamic charact...
Effects of twist, camber and thickness on aerodynamic features of 75-deg swept arrow win
Off-design aerodynamic characteristics of swept arrow wings with twist and camber at supersonic velo...
A cambered and twisted triangular wing of aspect ratio 2 in combination with a cambered body was inv...
Longitudinal stability and control characteristic of M wing aircraft at various Mach number
Wind tunnel tests of an arrow wing body configuration consisting of flat, twisted, and cambered twis...
Tabulation of wind tunnel pressure data and section aerodynamic characteristics for a reflex cambere...
This investigation is a continuation of the experimental and theoretical evaluation of blended wing-...
Wing models were tested in the high-speed section of the Langley Unitary Plan wind tunnel to study t...
Measurements were made of the lift, drag, and pitching moments on an arrow wing (taper ratio of zero...
An investigation of two semispan wings swept back 50 degrees 38 minutes was conducted in the Langley...
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
Effects of airfoil section shape and thickness on supersonic performance characteristics of wing bod...
Engine nacelle orientation effect on aerodynamic characteristics of arrow wing body configuratio
A series of arrow wings employing various degrees of twist and camber were tested in the Langley 4- ...
An investigation has been made at Mach numbers of 1.61 and 2.01 to determine the aerodynamic charact...
Effects of twist, camber and thickness on aerodynamic features of 75-deg swept arrow win
Off-design aerodynamic characteristics of swept arrow wings with twist and camber at supersonic velo...
A cambered and twisted triangular wing of aspect ratio 2 in combination with a cambered body was inv...
Longitudinal stability and control characteristic of M wing aircraft at various Mach number
Wind tunnel tests of an arrow wing body configuration consisting of flat, twisted, and cambered twis...
Tabulation of wind tunnel pressure data and section aerodynamic characteristics for a reflex cambere...
This investigation is a continuation of the experimental and theoretical evaluation of blended wing-...
Wing models were tested in the high-speed section of the Langley Unitary Plan wind tunnel to study t...
Measurements were made of the lift, drag, and pitching moments on an arrow wing (taper ratio of zero...
An investigation of two semispan wings swept back 50 degrees 38 minutes was conducted in the Langley...
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
Effects of airfoil section shape and thickness on supersonic performance characteristics of wing bod...
Engine nacelle orientation effect on aerodynamic characteristics of arrow wing body configuratio