NASA NTRS · 19840055181
Three-dimensional unsteady Euler equations solution using flux vector splitting
Abstract
A method for numerically solving the three-dimensional unsteady Euler equations using flux vector splitting is developed. The equations are cast in curvilinear coordinates and a finite volume discretization is used. An explicit upwind second-order predictor-corrector scheme is used to solve the discretized equations. The scheme is stable for a CFL number of 2 and local time stepping is used to accelerate convergence for steady-state problems. Characteristic variable boundary conditions are developed and used in the far-field and at surfaces. No additional dissipation terms are included in the scheme. Numerical results are compared with results from an existing three-dimensional Euler code and experimental data.
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Whitfield, D. L., Janus, J. M.. 1984-06-01. Three-dimensional unsteady Euler equations solution using flux vector splitting. https://ntrs.nasa.gov/citations/19840055181
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