Add to ORKGThe aerodynamic characteristics of wings with leading-edge vortex separation were predicted using a method based on a flow model with free vortex elements which are allowed to merge into a concentrated core. The calculated pressure distribution is more accurate than that predicted by methods with discrete vortex filaments alone. In addition, the computer time is reduced approximately by half
The aerodynamic characteristics of slender wings having separation induced vortex flows are investig...
The Boeing Commercial Airplane Company developed an inviscid three-dimensional lifting surface metho...
The many novel, innovative, and unique implementations and applications of the vortex-lattice method...
A method for predicting aerodynamic characteristics of slender wings with edge vortex separation was...
A method of predicting forces, moments, and detailed surface pressures on thin, sharp-edged wings wi...
A computer code base on an improved vortex filament/vortex core method for predicting aerodynamic ch...
A numerical method is developed to predict distributed and total aerodynamic characteristics for low...
A three-dimensional numerical model using vortex lattice methods (VLMs) is developed to solve the st...
An improved Nonlinear Vortex Lattice Method is presented to simulate steady and unsteady flows for w...
Separation-induced leading-edge vortices can dominate the flow about slender wings at moderate to hi...
Two simple wings were selected for study using the various implementations (old and new) of the vort...
We present a medium-fidelity aeroelastic framework for computing intermittently separating three-dim...
An examination of the potential flow computer code VSAERO to model leading edge separation over a de...
The quasi vortex-lattice method is reviewed and applied to the evaluation of backwash, with applicat...
Because the potential flow suction along the leading and side edges of a planform can be used to det...
The aerodynamic characteristics of slender wings having separation induced vortex flows are investig...
The Boeing Commercial Airplane Company developed an inviscid three-dimensional lifting surface metho...
The many novel, innovative, and unique implementations and applications of the vortex-lattice method...
A method for predicting aerodynamic characteristics of slender wings with edge vortex separation was...
A method of predicting forces, moments, and detailed surface pressures on thin, sharp-edged wings wi...
A computer code base on an improved vortex filament/vortex core method for predicting aerodynamic ch...
A numerical method is developed to predict distributed and total aerodynamic characteristics for low...
A three-dimensional numerical model using vortex lattice methods (VLMs) is developed to solve the st...
An improved Nonlinear Vortex Lattice Method is presented to simulate steady and unsteady flows for w...
Separation-induced leading-edge vortices can dominate the flow about slender wings at moderate to hi...
Two simple wings were selected for study using the various implementations (old and new) of the vort...
We present a medium-fidelity aeroelastic framework for computing intermittently separating three-dim...
An examination of the potential flow computer code VSAERO to model leading edge separation over a de...
The quasi vortex-lattice method is reviewed and applied to the evaluation of backwash, with applicat...
Because the potential flow suction along the leading and side edges of a planform can be used to det...
The aerodynamic characteristics of slender wings having separation induced vortex flows are investig...
The Boeing Commercial Airplane Company developed an inviscid three-dimensional lifting surface metho...
The many novel, innovative, and unique implementations and applications of the vortex-lattice method...