NASA NTRS · 19840021783
Acceleration to a steady state for the Euler equations
Abstract
A multi-stage Runge-Kutta method is analyzed for solving the Euler equations exterior to an airfoil. Highly subsonic, transonic and supersonic flows are evaluated. Various techniques for accelerating the convergence to a steady state are introduced and analyzed.
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Turkel, E.. 1984-07-01. Acceleration to a steady state for the Euler equations. https://ntrs.nasa.gov/citations/19840021783
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