NASA NTRS · 19920066370
Propulsion-related flowfields using the preconditioned Navier-Stokes equations
Abstract
A previous time-derivative preconditioning procedure for solving the Navier-Stokes is extended to the chemical species equations. The scheme is implemented using both the implicit ADI and the explicit Runge-Kutta algorithms. A new definition for time-step is proposed to enable grid-independent convergence. Several examples of both reacting and non-reacting propulsion-related flowfields are considered. In all cases, convergence that is superior to conventional methods is demonstrated. Accuracy is verified using the example of a backward facing step. These results demonstrate that preconditioning can enhance the capability of density-based methods over a wide range of Mach and Reynolds numbers.
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Venkateswaran, S., Weiss, J. M., Merkle, C. L., Choi, Y.-H.. 1992-07-01. Propulsion-related flowfields using the preconditioned Navier-Stokes equations. https://ntrs.nasa.gov/citations/19920066370
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