A method for computing inviscid hypersonic flow over complex configurations using unstructured meshes is presented. The unstructured grid solver uses and edge-based finite-volume formulation. Fluxes are computed using a flux-vector splitting scheme that is capable of representing constant enthalpy solutions..
A triangle-based unstructured finite volume method is developed for non-stationary chemically reacti...
Capturing strong shocks is a difficult task. It is also known that it leads to accuracy degradation ...
This paper addresses the solution of the compressible Euler equations on hexahedral meshes for super...
A method for computing inviscid hypersonic flow over complex configurations using unstructured meshe...
The paper describes a solver for the compressible inviscid flow equations which is based on a flux v...
Abstract: A comparison of five different spatial discretization schemes is performed considering a t...
This report describes the research work undertaken at the Massachusetts Institute of Technology. The...
Abstract:-The unsteady and inviscid compressible flow around a circular cylinder and airfoil has bee...
The synthesis of physical models for gas chemistry and turbulence from the structured grid codes LAU...
The mathematical and numerical formulation employed in the development of a new multi-dimensional Co...
A two-dimensional, axisymmetric, full Navier-Stokes solver has been developed with equilibrium and n...
A novel finite-volume formulation is proposed for unsteady solutions on complex geometries. A comput...
The present work implements the spectral finite volume scheme in a cell centered finite volume conte...
A novel unstructured shock-fitting algorithm for three-dimensional flows is proposed in this paper. ...
The use of unstructured mesh techniques for solving complex aerodynamic flows is discussed. The prin...
A triangle-based unstructured finite volume method is developed for non-stationary chemically reacti...
Capturing strong shocks is a difficult task. It is also known that it leads to accuracy degradation ...
This paper addresses the solution of the compressible Euler equations on hexahedral meshes for super...
A method for computing inviscid hypersonic flow over complex configurations using unstructured meshe...
The paper describes a solver for the compressible inviscid flow equations which is based on a flux v...
Abstract: A comparison of five different spatial discretization schemes is performed considering a t...
This report describes the research work undertaken at the Massachusetts Institute of Technology. The...
Abstract:-The unsteady and inviscid compressible flow around a circular cylinder and airfoil has bee...
The synthesis of physical models for gas chemistry and turbulence from the structured grid codes LAU...
The mathematical and numerical formulation employed in the development of a new multi-dimensional Co...
A two-dimensional, axisymmetric, full Navier-Stokes solver has been developed with equilibrium and n...
A novel finite-volume formulation is proposed for unsteady solutions on complex geometries. A comput...
The present work implements the spectral finite volume scheme in a cell centered finite volume conte...
A novel unstructured shock-fitting algorithm for three-dimensional flows is proposed in this paper. ...
The use of unstructured mesh techniques for solving complex aerodynamic flows is discussed. The prin...
A triangle-based unstructured finite volume method is developed for non-stationary chemically reacti...
Capturing strong shocks is a difficult task. It is also known that it leads to accuracy degradation ...
This paper addresses the solution of the compressible Euler equations on hexahedral meshes for super...
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