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.
Export citation and abstract BibTeX RIS
Content from this work may be used under the terms of the Creative Commons Attribution 3.0 licence. Any further distribution of this work must maintain attribution to the author(s) and the title of the work, journal citation and DOI.