Overset or Chimera grid approach is one of methods to cope with complex geometries. A spline based overset grid assembling system has been developed. The sys- tem is based on structured grid approach and covers comprehensive features for overset assembling, i.e., grid generation, grid modification, and computing Receptor-Donor Con- nectivity (RDC) for overset interpolation. Ferguson spline curve is used to compute curves through grid points and cell centers for trimming grids and computing RDC robustly and accurately. Flow simulation around Kriso Container Ship(KCS) with jointed grids shows good continuity of flow field between the grids. The overset grid assembling is enhanced to unsteady problem as dynamic ove...
University of Minnesota Ph.D. dissertation. December 2018. Major: Aerospace Engineering and Mechanic...
A deformable overset grid method was proposed to simulate the unsteady aerodynamic problems with mu...
A study of numerical attributes peculiar to an overset grid approach to unsteady aerodynamics predic...
The paper discusses the combined implementation of overset grid and patched grid methodologies and i...
Grid related issues of the Chimera overset grid method are discussed in the context of a method of s...
A deformable overset grid method is proposed to simulate the unsteady aerodynamic problems with mult...
A discussion of the strengths and weaknesses of overset composite grid and solution technology is gi...
The paper discusses the overset grid methodology implementation and its testing at transonic and sup...
Two approaches for CFD simulations for a complex geometry of a ship with an energy-saving duct ...
This progress report describes research performed to achieve algorithmic improvements in the use of ...
Unstructured grid technologies for hydrodynamic applications with bodies in relative motion and mesh...
Algorithms and computer code developments were performed for the overset grid approach to solving co...
AbstractIn this article, the overset grid assembly method is improved to efficiently solve several c...
Overset methods, by overlapping several grids, allow large and arbitrary motion of bodies. First dev...
\u3cp\u3eAn overset grid method for resolved simulation of incompressible (turbulent) flows around m...
University of Minnesota Ph.D. dissertation. December 2018. Major: Aerospace Engineering and Mechanic...
A deformable overset grid method was proposed to simulate the unsteady aerodynamic problems with mu...
A study of numerical attributes peculiar to an overset grid approach to unsteady aerodynamics predic...
The paper discusses the combined implementation of overset grid and patched grid methodologies and i...
Grid related issues of the Chimera overset grid method are discussed in the context of a method of s...
A deformable overset grid method is proposed to simulate the unsteady aerodynamic problems with mult...
A discussion of the strengths and weaknesses of overset composite grid and solution technology is gi...
The paper discusses the overset grid methodology implementation and its testing at transonic and sup...
Two approaches for CFD simulations for a complex geometry of a ship with an energy-saving duct ...
This progress report describes research performed to achieve algorithmic improvements in the use of ...
Unstructured grid technologies for hydrodynamic applications with bodies in relative motion and mesh...
Algorithms and computer code developments were performed for the overset grid approach to solving co...
AbstractIn this article, the overset grid assembly method is improved to efficiently solve several c...
Overset methods, by overlapping several grids, allow large and arbitrary motion of bodies. First dev...
\u3cp\u3eAn overset grid method for resolved simulation of incompressible (turbulent) flows around m...
University of Minnesota Ph.D. dissertation. December 2018. Major: Aerospace Engineering and Mechanic...
A deformable overset grid method was proposed to simulate the unsteady aerodynamic problems with mu...
A study of numerical attributes peculiar to an overset grid approach to unsteady aerodynamics predic...