Abstract: The present invention relates a numerical method to simulate the incompressible wing-tip vortex flows. This method is called Vorticity-Refinement, which refines the added vorticity as two different forms of force multiplied by two different factors to counteract the numerical diffusions in the numerical solutions by utilizing the high-order spatial discretization and improving the stability and convergence of the governing equations for incompressible flows.
Type:
Grant
Filed:
September 28, 2012
Date of Patent:
July 12, 2016
Assignee:
Xi'an Virtual-Dynamics Simulation Technology Inc.
Abstract: It is a numerical method for solving an inverse problem about the shape design of aerodynamic body in inviscid subsonic flows. This method transfers the original Euler equations into the stream-function plane, where it solves the Riemann problem across the streamline presenting the solid-wall and obtains the geometry of the solid-wall concurrently.
Type:
Grant
Filed:
September 18, 2012
Date of Patent:
July 5, 2016
Assignee:
Xi'an Virtual-Dynamics Simulation Technology Inc.