Add to ORKGHypersonic flight performance of basic and modified delta wings with diamond cross section
Slender sharp-edge wings having leading-edge sweep angles of 74 deg have been studied at Mach number...
Control surface effectiveness is an important parameter for any aeroplane. For a hypersonic aircraft...
Wind tunnel tests on aspect ratio 2.17 delta wing model with midchord boundary layer control flap
In order to indicate the effects of Reynolds number and other variables on the drag due to lift of d...
Effect of body cross sections and width-height ratio on performance of bodies and delta-wing- body c...
Hypersonic aerodynamic characteristics of delta wing x- 15 airplane configuration
Geometric modifications effect on lift-drag ratios of wing body configurations at hypersonic speed
A program to investigate the aerodynamic characteristics of a family of delta wings with a blunt dou...
Aerodynamic characteristics of thick delta wings at subsonic to supersonic speeds and angles of atta...
The models had aspect-ratio-2 diamond, delta, and arrow wings with the leading edges swept 45.00 deg...
The longitudinal, lateral, and directional aerodynamic characteristics of a delta-wing configuration...
An investigation has been conducted to explore the potential for optimizing airfoil shape at high su...
Aerodynamic characteristics in pitch of several wing-body combinations with wedge-shaped planform lo...
Rolling motion of 79-deg clipped delta wing configuration at supersonic speed - free flight investig...
An investigation of the aerodynamic performance of leading-edge flaps on three clipped delta and thr...
Slender sharp-edge wings having leading-edge sweep angles of 74 deg have been studied at Mach number...
Control surface effectiveness is an important parameter for any aeroplane. For a hypersonic aircraft...
Wind tunnel tests on aspect ratio 2.17 delta wing model with midchord boundary layer control flap
In order to indicate the effects of Reynolds number and other variables on the drag due to lift of d...
Effect of body cross sections and width-height ratio on performance of bodies and delta-wing- body c...
Hypersonic aerodynamic characteristics of delta wing x- 15 airplane configuration
Geometric modifications effect on lift-drag ratios of wing body configurations at hypersonic speed
A program to investigate the aerodynamic characteristics of a family of delta wings with a blunt dou...
Aerodynamic characteristics of thick delta wings at subsonic to supersonic speeds and angles of atta...
The models had aspect-ratio-2 diamond, delta, and arrow wings with the leading edges swept 45.00 deg...
The longitudinal, lateral, and directional aerodynamic characteristics of a delta-wing configuration...
An investigation has been conducted to explore the potential for optimizing airfoil shape at high su...
Aerodynamic characteristics in pitch of several wing-body combinations with wedge-shaped planform lo...
Rolling motion of 79-deg clipped delta wing configuration at supersonic speed - free flight investig...
An investigation of the aerodynamic performance of leading-edge flaps on three clipped delta and thr...
Slender sharp-edge wings having leading-edge sweep angles of 74 deg have been studied at Mach number...
Control surface effectiveness is an important parameter for any aeroplane. For a hypersonic aircraft...
Wind tunnel tests on aspect ratio 2.17 delta wing model with midchord boundary layer control flap