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NASA NTRS · 19920062933

Numerical simulations using a dynamic solution-adaptive grid algorithm, with applications to unsteady internal flows

Abstract

An investigation into the numerical simulation of unsteady flows is undertaken using a two-stage Runge-Kutta scheme coupled with the dynamic solution-adaptive grid algorithm developed by the authors. The inviscid fluxes are described by a modified Advective Upwind Split Method to eliminate the need for artificial dissipation. A well-documented numerical example containing moving discontinuities is presented that demonstrates the ability of the coupled grid/solver scheme to accurately capture unsteady flowfield phenomena. Applications are to a typical inlet diffuser configuration at Mach 3.0 with excessive back pressure inducing inlet unstart.

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Benson, Rusty A., Mcrae, D. S., Edwards, Jack R.. 1992-01-01. Numerical simulations using a dynamic solution-adaptive grid algorithm, with applications to unsteady internal flows. https://ntrs.nasa.gov/citations/19920062933

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