Add to ORKGEquations for the semianalytic representation of a class of surfaces that vary smoothly in cross-sectional shape are presented. Some methods of fitting together and superimposing such surfaces are described. A brief discussion is also included of the application of the theory in various contexts such as computerized lofting of aerodynamic surfaces and grid generation
A novel (geometrical) parametrization procedure using solutions to a suitably chosen fourth order pa...
In the aircraft industry, shape optimization is fast becoming a major component of aerodynamic desig...
Most of the work accomplished on surface blending is based on visual trimming. In the process of vis...
A computer program developed to fit smooth surfaces to the component parts of three-dimensional airc...
A novel (geometrical) parametrization procedure using solutions to a suitably chosen fourth order pa...
(Maximum 200 words) A theory for representing a parameter-dependent function as a function trajecto...
A surface-fitting technique has been developed which addresses two problems with existing geometry p...
Class-Shape Transformation (CST) is a popular method for creating analytical representations of the ...
Numerical results illustrating the capabilities of an advanced aerodynamic surface paneling method a...
A theory for representing a parameter-dependent function as a function trajectory is described. Addi...
The geometry of general three-dimensional bodies is generated from coordinates of points in several ...
Algebraic procedures are described for the automatic generation of structured, single-block flow com...
A fast and versatile procedure for algebraically generating boundary conforming computational grids ...
A parametric model is presented for the blended-wing-body airplane, one concept being proposed for t...
Detailed descriptions are given of the theoretical methods and associated computer codes of a progra...
A novel (geometrical) parametrization procedure using solutions to a suitably chosen fourth order pa...
In the aircraft industry, shape optimization is fast becoming a major component of aerodynamic desig...
Most of the work accomplished on surface blending is based on visual trimming. In the process of vis...
A computer program developed to fit smooth surfaces to the component parts of three-dimensional airc...
A novel (geometrical) parametrization procedure using solutions to a suitably chosen fourth order pa...
(Maximum 200 words) A theory for representing a parameter-dependent function as a function trajecto...
A surface-fitting technique has been developed which addresses two problems with existing geometry p...
Class-Shape Transformation (CST) is a popular method for creating analytical representations of the ...
Numerical results illustrating the capabilities of an advanced aerodynamic surface paneling method a...
A theory for representing a parameter-dependent function as a function trajectory is described. Addi...
The geometry of general three-dimensional bodies is generated from coordinates of points in several ...
Algebraic procedures are described for the automatic generation of structured, single-block flow com...
A fast and versatile procedure for algebraically generating boundary conforming computational grids ...
A parametric model is presented for the blended-wing-body airplane, one concept being proposed for t...
Detailed descriptions are given of the theoretical methods and associated computer codes of a progra...
A novel (geometrical) parametrization procedure using solutions to a suitably chosen fourth order pa...
In the aircraft industry, shape optimization is fast becoming a major component of aerodynamic desig...
Most of the work accomplished on surface blending is based on visual trimming. In the process of vis...