Add to ORKGSome of the theoretical and experimental research conducted at the NASA Langley Research Center is presented to investigate the subsonic vortex-lift producing capabilities for two classes of Super-Cruise designs: a close-coupled wing-canard arrangement and a slender wing configuration. In addition, several analytical methods are discussed for estimating critical structural design loads for thin, highly swept wings having separated leading-edge vortex flows
Exploratory wind tunnel tests are reported on a 74 deg. delta wing model. The potential of a vortex ...
An extension of the suction analogy for the estimation of vortex lift along the side edge of wings i...
The linear lifting surface theory which predicts the life in supersonic flow, even though the drag i...
The Boeing Commercial Airplane Company developed an inviscid three-dimensional lifting surface metho...
Accomplishments in vortex flap research are summarized. A singular feature of the vortex flap is tha...
A theoretical and experimental investigation was conducted of the subsonic maneuver capability of a ...
Wind tunnel tests were conducted to examine the use of wing leading-edge devices for improved subson...
A wind tunnel investigation was conducted to study the application of supercritical technology to hi...
Wind-tunnel studies at the Langley Research Center have shown that significant increases in maximum ...
Technical progress made in each of the disciplinary research areas affecting the design of supersoni...
A theoretical and experimental program in which a wing concept for supersonic maneuvering was develo...
An investigation was conducted in the NASA Langley 8-foot transonic pressure tunnel at Mach numbers ...
A wind tunnel test where load distributions were obtained at transonic speeds on both the canard and...
Results of the experimental validation are presented for the three dimensional cambered wing which w...
A fully three-dimensional subsonic panel method that can handle arbitrary shed vortex wakes is used ...
Exploratory wind tunnel tests are reported on a 74 deg. delta wing model. The potential of a vortex ...
An extension of the suction analogy for the estimation of vortex lift along the side edge of wings i...
The linear lifting surface theory which predicts the life in supersonic flow, even though the drag i...
The Boeing Commercial Airplane Company developed an inviscid three-dimensional lifting surface metho...
Accomplishments in vortex flap research are summarized. A singular feature of the vortex flap is tha...
A theoretical and experimental investigation was conducted of the subsonic maneuver capability of a ...
Wind tunnel tests were conducted to examine the use of wing leading-edge devices for improved subson...
A wind tunnel investigation was conducted to study the application of supercritical technology to hi...
Wind-tunnel studies at the Langley Research Center have shown that significant increases in maximum ...
Technical progress made in each of the disciplinary research areas affecting the design of supersoni...
A theoretical and experimental program in which a wing concept for supersonic maneuvering was develo...
An investigation was conducted in the NASA Langley 8-foot transonic pressure tunnel at Mach numbers ...
A wind tunnel test where load distributions were obtained at transonic speeds on both the canard and...
Results of the experimental validation are presented for the three dimensional cambered wing which w...
A fully three-dimensional subsonic panel method that can handle arbitrary shed vortex wakes is used ...
Exploratory wind tunnel tests are reported on a 74 deg. delta wing model. The potential of a vortex ...
An extension of the suction analogy for the estimation of vortex lift along the side edge of wings i...
The linear lifting surface theory which predicts the life in supersonic flow, even though the drag i...