A simple and efficient moving grid technique is proposed for computing unsteady flow problems with geometrical deformation, relative body movement or shape changes due to aerodynamic optimisation and fluid-structure interaction. A Delaunay graph of the solution domain is first generated, which can be moved easily during the geometric dynamic deformation, even for very large distortion. A one to one mapping between the Delaunay graph and the computational grid is maintained during the movement. The new computational grid after the dynamic movement can be generated efficiently through the mapping while maintaining the primary qualities of the grid. While most dynamic grid deformation techniques are iterative based on the spring analogy, the p...
A new point-by-point mesh movement algorithm is developed for the deformation of unstructured grids....
An unsteady Reynolds-averaged Navier-Stokes solver for unstructured grids has been extended to handl...
A new, efficient, and at the same time most precise calculation method for unsteady aerodynamics is ...
A simple and efficient dynamic grid deformation technique is proposed for computing unsteady flow pr...
Dynamic grid algorithm is essential for numerical simulation of fluid-structure interaction problems...
A deformable overset grid method was proposed to simulate the unsteady aerodynamic problems with mu...
Abstract: Numerical simulation of the aeroelastic behaviour of wings and rotor blades requires the c...
AbstractA mesh deformation algorithm for unstructured Cartesian grids is presented. Given a surface ...
An eective dynamic moving mesh algorithm suitable for multiblock parallel unsteady ow calculations ...
A novel parallel dynamic moving mesh algorithm designed for multiblock parallel unsteady ow calcula...
Moving grid or mesh deformation is a challenging task for numerical simulation of fluid-structure in...
International audienceThree-dimensional real-life simulations are generally unsteady and involve mov...
AbstractThree-dimensional real-life simulations are generally unsteady and involve moving geometries...
The most difficult part of the solution process for the flowing problems between t1uid and structure...
A deformable overset grid method is proposed to simulate the unsteady aerodynamic problems with mult...
A new point-by-point mesh movement algorithm is developed for the deformation of unstructured grids....
An unsteady Reynolds-averaged Navier-Stokes solver for unstructured grids has been extended to handl...
A new, efficient, and at the same time most precise calculation method for unsteady aerodynamics is ...
A simple and efficient dynamic grid deformation technique is proposed for computing unsteady flow pr...
Dynamic grid algorithm is essential for numerical simulation of fluid-structure interaction problems...
A deformable overset grid method was proposed to simulate the unsteady aerodynamic problems with mu...
Abstract: Numerical simulation of the aeroelastic behaviour of wings and rotor blades requires the c...
AbstractA mesh deformation algorithm for unstructured Cartesian grids is presented. Given a surface ...
An eective dynamic moving mesh algorithm suitable for multiblock parallel unsteady ow calculations ...
A novel parallel dynamic moving mesh algorithm designed for multiblock parallel unsteady ow calcula...
Moving grid or mesh deformation is a challenging task for numerical simulation of fluid-structure in...
International audienceThree-dimensional real-life simulations are generally unsteady and involve mov...
AbstractThree-dimensional real-life simulations are generally unsteady and involve moving geometries...
The most difficult part of the solution process for the flowing problems between t1uid and structure...
A deformable overset grid method is proposed to simulate the unsteady aerodynamic problems with mult...
A new point-by-point mesh movement algorithm is developed for the deformation of unstructured grids....
An unsteady Reynolds-averaged Navier-Stokes solver for unstructured grids has been extended to handl...
A new, efficient, and at the same time most precise calculation method for unsteady aerodynamics is ...