Add to ORKGThe many novel, innovative, and unique implementations and applications of the vortex-lattice method to aerodynamic design and analysis which have been performed by Industry, Government, and Universities were presented. Although this analytical tool is not new, it continues to be utilized and refined in the aeronautical community
The program was designed to provide solutions of engineering accuracy for determining the aerodynami...
Computer program for estimating subsonic aerodynamic characteristics of various aerodynamic configur...
The latest production version, MARK IV, of the NASA-Langley vortex lattice computer program is summa...
This paper presents a new non-linear formulation of the classical Vortex Lattice Method (VLM) approa...
This paper presents a new non-linear formulation of the classical Vortex Lattice Method (VLM) approa...
This paper presents a new non-linear formulation of the classical Vortex Lattice Method (VLM) approa...
Vortex-lattice FORTRAN program for estimating subsonic aerodynamic characteristics of complex planfo...
A three-dimensional numerical model using vortex lattice methods (VLMs) is developed to solve the st...
Nonlinear panel methods have no proof for the existence and uniqueness of their solutions. The conve...
Two simple wings were selected for study using the various implementations (old and new) of the vort...
The applicability of the vortex lattice method to the design of human powered aircraft is investigat...
A new subsonic method has been developed by which the mean camber surface can be determined for trim...
The close-approach problem associated with flow calculation methods based on vortex-lattice theory w...
The SUGAR Truss-BracedWing (TBW) aircraft concept is a Boeing-developed N+3 aircraft configuration f...
An integrated aerodynamic optimization technique based on vortex lattice theory is being proposed. T...
The program was designed to provide solutions of engineering accuracy for determining the aerodynami...
Computer program for estimating subsonic aerodynamic characteristics of various aerodynamic configur...
The latest production version, MARK IV, of the NASA-Langley vortex lattice computer program is summa...
This paper presents a new non-linear formulation of the classical Vortex Lattice Method (VLM) approa...
This paper presents a new non-linear formulation of the classical Vortex Lattice Method (VLM) approa...
This paper presents a new non-linear formulation of the classical Vortex Lattice Method (VLM) approa...
Vortex-lattice FORTRAN program for estimating subsonic aerodynamic characteristics of complex planfo...
A three-dimensional numerical model using vortex lattice methods (VLMs) is developed to solve the st...
Nonlinear panel methods have no proof for the existence and uniqueness of their solutions. The conve...
Two simple wings were selected for study using the various implementations (old and new) of the vort...
The applicability of the vortex lattice method to the design of human powered aircraft is investigat...
A new subsonic method has been developed by which the mean camber surface can be determined for trim...
The close-approach problem associated with flow calculation methods based on vortex-lattice theory w...
The SUGAR Truss-BracedWing (TBW) aircraft concept is a Boeing-developed N+3 aircraft configuration f...
An integrated aerodynamic optimization technique based on vortex lattice theory is being proposed. T...
The program was designed to provide solutions of engineering accuracy for determining the aerodynami...
Computer program for estimating subsonic aerodynamic characteristics of various aerodynamic configur...
The latest production version, MARK IV, of the NASA-Langley vortex lattice computer program is summa...