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NASA NTRS · 19740027801

Time-split finite-volume method for three-dimensional blunt-body flow

Abstract

An efficient numerical method for calculating plane, axisymmetric, and fully three-dimensional blunt-body flow is presented. It is a second-order-accurate, time-dependent finite-volume procedure that solves the Euler equations in integral conservation-law form. These equations are written with respect to a Cartesian coordinate system in which an embedded mesh adjusts in time to the motion of the bow shock that is automatically captured as part of the weak solution. With such an adjusting mesh, oscillations in flow properties near the shock are shown to be virtually eliminated. The scheme uses a time-splitting concept that accelerates the convergence appreciably. Comparisons are made between computed and experimental results.

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BibTeXRIS

Rizzi, A. W., Inouye, M.. 1973-11-01. Time-split finite-volume method for three-dimensional blunt-body flow. https://ntrs.nasa.gov/citations/19740027801

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