A methodology for accurate and efficient simulation of unsteady, compressible flows is presented. The cornerstones of the methodology are a special discretization of the Navier-Stokes equations on structured body-fitted grid systems and an efficient solution-adaptive mesh refinement technique for structured grids. The discretization employs an explicit multidimensional upwind scheme for the inviscid fluxes and an implicit treatment of the viscous terms. The mesh refinement technique is based on the AMR algorithm of Berger and Colella. In this approach, cells on each level of refinement are organized into a small number of topologically rectangular blocks, each containing several thousand cells. The small number of blocks leads to small over...
A Cartesian cell-based approach for adaptively refined solutions of the Euler and Navier-Stokes equa...
A space-time adaptive gridding technique for unsteady flows is presented. The technique is applied t...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77313/1/AIAA-13171-269.pd
A numerical scheme for simulation of unsteady, viscous, compressible flows is considered. The scheme...
A method for simulating two-dimensional, high-Reynolds-number, compressible flows about complex geom...
The use of unstructured mesh techniques for solving complex aerodynamic flows is discussed. The prin...
New 2D and 3D unstructured-grid based flow solvers have been developed for simulating steady compres...
A general purpose unstructured mesh solver for steady-state two-dimensional inviscid and viscous flo...
During the past two decades, there has been significant progress in the field of numerical simulatio...
An upwinding flux difference splitting method has been used to solve the Euler equations for compre...
To be truly compatible with structured grids, an AMR algorithm should employ a block structure for t...
Grid convergence of several high order methods for the computation of rapidly developing complex uns...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76130/1/AIAA-1992-443-336.pd
The Navier-Stokes equations are solved numerically for two-dimensional steady viscous laminar flows....
University of Minnesota Ph.D. dissertation. August 2015. Major: Aerospace Engineering and Mechanics....
A Cartesian cell-based approach for adaptively refined solutions of the Euler and Navier-Stokes equa...
A space-time adaptive gridding technique for unsteady flows is presented. The technique is applied t...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77313/1/AIAA-13171-269.pd
A numerical scheme for simulation of unsteady, viscous, compressible flows is considered. The scheme...
A method for simulating two-dimensional, high-Reynolds-number, compressible flows about complex geom...
The use of unstructured mesh techniques for solving complex aerodynamic flows is discussed. The prin...
New 2D and 3D unstructured-grid based flow solvers have been developed for simulating steady compres...
A general purpose unstructured mesh solver for steady-state two-dimensional inviscid and viscous flo...
During the past two decades, there has been significant progress in the field of numerical simulatio...
An upwinding flux difference splitting method has been used to solve the Euler equations for compre...
To be truly compatible with structured grids, an AMR algorithm should employ a block structure for t...
Grid convergence of several high order methods for the computation of rapidly developing complex uns...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76130/1/AIAA-1992-443-336.pd
The Navier-Stokes equations are solved numerically for two-dimensional steady viscous laminar flows....
University of Minnesota Ph.D. dissertation. August 2015. Major: Aerospace Engineering and Mechanics....
A Cartesian cell-based approach for adaptively refined solutions of the Euler and Navier-Stokes equa...
A space-time adaptive gridding technique for unsteady flows is presented. The technique is applied t...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77313/1/AIAA-13171-269.pd