A fast algorithm to solve viscous two-phase flow in an axisymmetric rocket nozzle
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Publication:4221531
DOI<501::AID-FLD642>3.0.CO;2-U 10.1002/(SICI)1097-0363(19980315)26:5<501::AID-FLD642>3.0.CO;2-UzbMath0921.76110OpenAlexW1989196773MaRDI QIDQ4221531
Publication date: 11 April 1999
Full work available at URL: https://doi.org/10.1002/(sici)1097-0363(19980315)26:5<501::aid-fld642>3.0.co;2-u
finite volume methodcompressible flowsgas-particle flowstructured gridsEulerian-Eulerian approachBaldwin-Lomax modelmultistage time-stepping Runge-Kutta scheme
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