Add to ORKGEffects of twist, camber and thickness on aerodynamic features of 75-deg swept arrow win
Longitudinal stability and control characteristic of M wing aircraft at various Mach number
Slender sharp-edge wings having leading-edge sweep angles of 74 deg have been studied at Mach number...
Measurements were made of the lift, drag, and pitching moments on an arrow wing (taper ratio of zero...
Off-design aerodynamic characteristics of swept arrow wings with twist and camber at supersonic velo...
An investigation has been made at Mach numbers of 1.61 and 2.01 to determine the aerodynamic charact...
A series of arrow wings employing various degrees of twist and camber were tested in the Langley 4- ...
Profile change effects on aerodynamic characteristics of twisted and cambered arrow wing at superson...
Wing models were tested in the high-speed section of the Langley Unitary Plan wind tunnel to study t...
An investigation of two semispan wings swept back 50 degrees 38 minutes was conducted in the Langley...
This investigation is a continuation of the experimental and theoretical evaluation of blended wing-...
Data are provided for the evaluation of the aerodynamic performance of a series of twisted and cambe...
The longitudinal aerodynamic characteristics of a 35 deg swept, variable camber and twist semispan w...
Effects of airfoil section shape and thickness on supersonic performance characteristics of wing bod...
Tabulation of wind tunnel pressure data and section aerodynamic characteristics for a reflex cambere...
Wind tunnel tests of an arrow wing body configuration consisting of flat, twisted, and cambered twis...
Longitudinal stability and control characteristic of M wing aircraft at various Mach number
Slender sharp-edge wings having leading-edge sweep angles of 74 deg have been studied at Mach number...
Measurements were made of the lift, drag, and pitching moments on an arrow wing (taper ratio of zero...
Off-design aerodynamic characteristics of swept arrow wings with twist and camber at supersonic velo...
An investigation has been made at Mach numbers of 1.61 and 2.01 to determine the aerodynamic charact...
A series of arrow wings employing various degrees of twist and camber were tested in the Langley 4- ...
Profile change effects on aerodynamic characteristics of twisted and cambered arrow wing at superson...
Wing models were tested in the high-speed section of the Langley Unitary Plan wind tunnel to study t...
An investigation of two semispan wings swept back 50 degrees 38 minutes was conducted in the Langley...
This investigation is a continuation of the experimental and theoretical evaluation of blended wing-...
Data are provided for the evaluation of the aerodynamic performance of a series of twisted and cambe...
The longitudinal aerodynamic characteristics of a 35 deg swept, variable camber and twist semispan w...
Effects of airfoil section shape and thickness on supersonic performance characteristics of wing bod...
Tabulation of wind tunnel pressure data and section aerodynamic characteristics for a reflex cambere...
Wind tunnel tests of an arrow wing body configuration consisting of flat, twisted, and cambered twis...
Longitudinal stability and control characteristic of M wing aircraft at various Mach number
Slender sharp-edge wings having leading-edge sweep angles of 74 deg have been studied at Mach number...
Measurements were made of the lift, drag, and pitching moments on an arrow wing (taper ratio of zero...