Add to ORKGSome ideas for using hodograph theory, mapping techniques and methods of characteristics to formulate typical aerodynamic design boundary value problems are developed. The inverse method of characteristics is shown to be a fast tool for design of transonic flow elements as well as supersonic flows with given shock waves
Advances in inverse design and optimization theory in engineering fields in China are presented. Two...
This thesis describes the development of two inverse design methods, suitable for designing two- and...
Abstract: The development and application of a three-dimensional inverse methodology in which the bl...
Progress in the use of the Hodograph method of aerodynamic design is discussed. It was found that th...
The direct-inverse technique was developed into a numerical method, called TRANDES, that is suitable...
A direct-inverse approach to the transonic design problem was presented in its initial state at the ...
An inverse method for turbomachinery blade design is presented along with the three-dimensional turb...
A numerical technique for designing transonic airfoils having a prescribed pressure distribution (th...
A numerical technique to generate cascades is presented. The basic prescribed parameters are: inlet ...
In the present work an extension of an aerodynamic optimization system for inverse design is carried...
The aerodynamic design of classical and innovative nozzle concepts is investigated by an inverse me...
Given the current level of jet engine performance, improvement of the various turbomachinery compone...
Aerodynamic characteristics are very sensitive to airfoil leading-edge geometry, and its accurate tr...
An inverse method, which works for full 3D viscous applications in turbomachinery aerodynamic design...
A numerical technique to solve two-dimensional inverse problems that arise in aerodynamic design is ...
Advances in inverse design and optimization theory in engineering fields in China are presented. Two...
This thesis describes the development of two inverse design methods, suitable for designing two- and...
Abstract: The development and application of a three-dimensional inverse methodology in which the bl...
Progress in the use of the Hodograph method of aerodynamic design is discussed. It was found that th...
The direct-inverse technique was developed into a numerical method, called TRANDES, that is suitable...
A direct-inverse approach to the transonic design problem was presented in its initial state at the ...
An inverse method for turbomachinery blade design is presented along with the three-dimensional turb...
A numerical technique for designing transonic airfoils having a prescribed pressure distribution (th...
A numerical technique to generate cascades is presented. The basic prescribed parameters are: inlet ...
In the present work an extension of an aerodynamic optimization system for inverse design is carried...
The aerodynamic design of classical and innovative nozzle concepts is investigated by an inverse me...
Given the current level of jet engine performance, improvement of the various turbomachinery compone...
Aerodynamic characteristics are very sensitive to airfoil leading-edge geometry, and its accurate tr...
An inverse method, which works for full 3D viscous applications in turbomachinery aerodynamic design...
A numerical technique to solve two-dimensional inverse problems that arise in aerodynamic design is ...
Advances in inverse design and optimization theory in engineering fields in China are presented. Two...
This thesis describes the development of two inverse design methods, suitable for designing two- and...
Abstract: The development and application of a three-dimensional inverse methodology in which the bl...