Add to ORKGThe lateral-directional characteristics for configurations with vortex flaps were calculated by the VORSTAB code. In view of the poor correlation between the VORSTABL results and the data, it was decided to examine in detail the reasons behind the discrepancy. After corrections in the data, the characteristics were recalculated. The prediction of dihedral effect is now largely improved
Three different numerical codes are employed to determine the aerodynamic characteristics of wings w...
An experimental study was conducted in the Virginia Tech Stability Wind Tunnel to determine surface ...
A user's manual is presented for a computer program in which a vortex-lattice lifting-surface method...
The low speed lateral/directional characteristics of a generic 74 degree delta wing body configurati...
A computer program based on the Quasi-Vortex-Lattice Method of Lan is presented for calculating long...
Calculation of longitudinal and lateral directional aerodynamic characteristics of airplanes by the ...
A wind tunnel study at Mach 0.4 was conducted for a slender wing-body configuration with a leading e...
Accomplishments in vortex flap research are summarized. A singular feature of the vortex flap is tha...
The linear lifting surface theory which predicts the life in supersonic flow, even though the drag i...
An investigation was made into the drag reduction capability of vortex tabs on delta wing vortex fla...
Flow visualization studies were conducted to qualitatively determine the effects of active generatio...
The nonplanar quasi-vortex-lattice method is applied to the calculation of lateral-directional stabi...
An engineering method for predicting the longitudinal aerodynamic characteristics of wing-flap confi...
Exploratory wind tunnel tests are reported on a 74 deg. delta wing model. The potential of a vortex ...
Tests were conducted in the Langley 12-foot low-speed wind-tunnel to determine the longitudinal and ...
Three different numerical codes are employed to determine the aerodynamic characteristics of wings w...
An experimental study was conducted in the Virginia Tech Stability Wind Tunnel to determine surface ...
A user's manual is presented for a computer program in which a vortex-lattice lifting-surface method...
The low speed lateral/directional characteristics of a generic 74 degree delta wing body configurati...
A computer program based on the Quasi-Vortex-Lattice Method of Lan is presented for calculating long...
Calculation of longitudinal and lateral directional aerodynamic characteristics of airplanes by the ...
A wind tunnel study at Mach 0.4 was conducted for a slender wing-body configuration with a leading e...
Accomplishments in vortex flap research are summarized. A singular feature of the vortex flap is tha...
The linear lifting surface theory which predicts the life in supersonic flow, even though the drag i...
An investigation was made into the drag reduction capability of vortex tabs on delta wing vortex fla...
Flow visualization studies were conducted to qualitatively determine the effects of active generatio...
The nonplanar quasi-vortex-lattice method is applied to the calculation of lateral-directional stabi...
An engineering method for predicting the longitudinal aerodynamic characteristics of wing-flap confi...
Exploratory wind tunnel tests are reported on a 74 deg. delta wing model. The potential of a vortex ...
Tests were conducted in the Langley 12-foot low-speed wind-tunnel to determine the longitudinal and ...
Three different numerical codes are employed to determine the aerodynamic characteristics of wings w...
An experimental study was conducted in the Virginia Tech Stability Wind Tunnel to determine surface ...
A user's manual is presented for a computer program in which a vortex-lattice lifting-surface method...