| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 763109 | Computers & Fluids | 2009 | 12 Pages |
Abstract
A new floating shock-fitting technique featuring the explicit computation of shocks by means of the Rankine–Hugoniot relations has been implemented on two-dimensional unstructured grids. This paper illustrates the algorithmic features of this original technique and the results obtained in the computation of the hypersonic flow past a circular cylinder and a steady Mach reflection.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
Authors
Renato Paciorri, Aldo Bonfiglioli,