Abstract
A three-dimensional finite element Navier-Stokes solver has been developed for calculating transonic viscous flow on unstructured grids about complex aerodynamic configurations. The solver employs a second-orderaccurate space discretization of the Navier-Stokes equations obtained from a Galerkin weighted-residual approximation. Time discretization is obtained using either an explicit two-step Lax-Wendroff scheme, or an explicit multistep Runge-Kutta scheme. Boundary conditions are implemented using a procedure based on the method of characteristics. The overall solution procedure has been initially validated by calculating two- and three-dimensional inviscid and viscous transonic flows.
Original language | English |
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Pages (from-to) | 648-654 |
Number of pages | 7 |
Journal | AIAA Journal |
Volume | 30 |
Issue number | 3 |
DOIs | |
State | Published - Mar 1992 |