NASA NTRS · 19890030080
A spectral multi-domain technique for viscous compressible reacting flows
Abstract
The first application of a spectral multidomain method for viscous compressible flow is presented. The method imposes a global flux balance condition at the interface so that high-order continuity of the solution is preserved. The solution scheme can be adapted to the particular requirement in each subdomain. To illustrate these advantages, a Mach 11 shock calculation is presented to study the chemical kinetics initiated as air passes through a fully resolved shock wave.
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Macaraeg, M. G., Streett, C. L.. 1988-10-01. A spectral multi-domain technique for viscous compressible reacting flows. https://ntrs.nasa.gov/citations/19890030080
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