A deformable overset grid method is proposed to simulate the unsteady aerodynamic problems with multiple flexible moving bodies. This method uses an unstructured overset grid coupled with local mesh deformation to achieve both robustness and efficiency. The overset grid hierarchically organizes the subgrids into clusters and layers, allowing for overlapping/embedding of different type meshes, in which the mesh quality and resolution can be independently controlled. At each time step, mesh deformation is locally applied to the subgrids associated with deforming bodies by an improved Delaunay graph mapping method that uses a very coarse Delaunay mesh as the background graph. The graph is moved and deformed by the spring analogy method accordi...
[Abstract] A method of unstructured dynamic overset grids is developed for the simulation of rotor f...
This progress report describes research performed to achieve algorithmic improvements in the use of ...
High-fidelity flight maneuver simulations are crucial for the development of realistic digital aircr...
A deformable overset grid method was proposed to simulate the unsteady aerodynamic problems with mu...
University of Minnesota Ph.D. dissertation. December 2018. Major: Aerospace Engineering and Mechanic...
Unstructured grid technologies for hydrodynamic applications with bodies in relative motion and mesh...
A conservative overset mesh scheme has been developed for the simulation of unsteady time-accurate f...
A simple and efficient moving grid technique is proposed for computing unsteady flow problems with g...
A flapping NACA0012 wing with spanwise rigid and flexible configurations is simulated using the Dela...
A simple and efficient dynamic grid deformation technique is proposed for computing unsteady flow pr...
An unsteady Reynolds-averaged Navier-Stokes solver for unstructured grids has been extended to handl...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76229/1/AIAA-1993-3391-356.pd
AbstractIn the design process of rocket, airplane and store separation systems, the aerodynamic of m...
Overset or Chimera grid approach is one of methods to cope with complex geometries. A spline bas...
The paper discusses the overset grid methodology implementation and its testing at transonic and sup...
[Abstract] A method of unstructured dynamic overset grids is developed for the simulation of rotor f...
This progress report describes research performed to achieve algorithmic improvements in the use of ...
High-fidelity flight maneuver simulations are crucial for the development of realistic digital aircr...
A deformable overset grid method was proposed to simulate the unsteady aerodynamic problems with mu...
University of Minnesota Ph.D. dissertation. December 2018. Major: Aerospace Engineering and Mechanic...
Unstructured grid technologies for hydrodynamic applications with bodies in relative motion and mesh...
A conservative overset mesh scheme has been developed for the simulation of unsteady time-accurate f...
A simple and efficient moving grid technique is proposed for computing unsteady flow problems with g...
A flapping NACA0012 wing with spanwise rigid and flexible configurations is simulated using the Dela...
A simple and efficient dynamic grid deformation technique is proposed for computing unsteady flow pr...
An unsteady Reynolds-averaged Navier-Stokes solver for unstructured grids has been extended to handl...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76229/1/AIAA-1993-3391-356.pd
AbstractIn the design process of rocket, airplane and store separation systems, the aerodynamic of m...
Overset or Chimera grid approach is one of methods to cope with complex geometries. A spline bas...
The paper discusses the overset grid methodology implementation and its testing at transonic and sup...
[Abstract] A method of unstructured dynamic overset grids is developed for the simulation of rotor f...
This progress report describes research performed to achieve algorithmic improvements in the use of ...
High-fidelity flight maneuver simulations are crucial for the development of realistic digital aircr...