Abstract
We propose a numerical method for a supersonic van der Waals gas flow about a round cone. This method enables one to calculate shock waves attached to the cone and flow parameters between the shock wave and the surface area of the cone. The advantages of the algorithm are demonstrated on some examples.
Original language | English |
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Article number | 012009 |
Number of pages | 7 |
Journal | Journal of Physics: Conference Series |
Volume | 894 |
Issue number | 1 |
DOIs | |
Publication status | Published - 22 Oct 2017 |