NASA NTRS · 19860037945
A shock capturing technique for hypersonic, chemically relaxing flows
Abstract
A fully coupled, shock capturing technique is presented for chemically reacting flows at high Mach numbers. The technique makes use of a total variation diminishing (TVD) dissipation operator which results in sharp, crisp shocks. The eigenvalues and eigenvectors of the fully coupled system, which includes species conversion equations in addition to the gas dynamics equations, are analytically derived for a general reacting gas. Species production terms for a model dissociating gas are introduced and are included in the algorithm. The convective terms are solved using a first-order TVD scheme while the source terms are solved using a fourth-order Runge-Kutta scheme to enhance stability. Results from one-dimensional numerical experiments are shown for a two species and a three species gas.
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Eberhardt, S., Brown, K.. 1986-01-01. A shock capturing technique for hypersonic, chemically relaxing flows. https://ntrs.nasa.gov/citations/19860037945
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