A Time-Accurate Adaptive Grid Method and the Numerical Simulation of a Shock-Vortex Interaction

A Time-Accurate Adaptive Grid Method and the Numerical Simulation of a Shock-Vortex Interaction
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
Total Pages: 24
Release: 2018-06-29
Genre:
ISBN: 9781722038182

A time accurate, general purpose, adaptive grid method is developed that is suitable for multidimensional steady and unsteady numerical simulations. The grid point movement is performed in a manner that generates smooth grids which resolve the severe solution gradients and the sharp transitions in the solution gradients. The temporal coupling of the adaptive grid and the PDE solver is performed with a grid prediction correction method that is simple to implement and ensures the time accuracy of the grid. Time accurate solutions of the 2-D Euler equations for an unsteady shock vortex interaction demonstrate the ability of the adaptive method to accurately adapt the grid to multiple solution features. Bockelie, Michael J. and Eiseman, Peter R. Langley Research Center AF-AFOSR-0307-86; NAG1-427; RTOP 505-90-21-02...

A Time-Accurate Adaptive Grid Method and the Numerical Simulation of a Shock-Vortex Interaction

A Time-Accurate Adaptive Grid Method and the Numerical Simulation of a Shock-Vortex Interaction
Author: National Aeronautics and Space Adm Nasa
Publisher:
Total Pages: 26
Release: 2018-10-23
Genre:
ISBN: 9781729146187

A time accurate, general purpose, adaptive grid method is developed that is suitable for multidimensional steady and unsteady numerical simulations. The grid point movement is performed in a manner that generates smooth grids which resolve the severe solution gradients and the sharp transitions in the solution gradients. The temporal coupling of the adaptive grid and the PDE solver is performed with a grid prediction correction method that is simple to implement and ensures the time accuracy of the grid. Time accurate solutions of the 2-D Euler equations for an unsteady shock vortex interaction demonstrate the ability of the adaptive method to accurately adapt the grid to multiple solution features. Bockelie, Michael J. and Eiseman, Peter R. Langley Research Center AF-AFOSR-0307-86; NAG1-427; RTOP 505-90-21-02

NASA Technical Paper

NASA Technical Paper
Author: United States. National Aeronautics and Space Administration
Publisher:
Total Pages: 380
Release: 1990
Genre: Aeronautics
ISBN: