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Volume of Fluid method for low-Mach-number compressible supercritical liquid jet
2021
International Conference on Liquid Atomization and Spray Systems (ICLASS)
A two-phase, low-Mach-number compressible flow solver is proposed. Density variations are linked to changes in composition and temperature rather than pressure. The interface is tracked using a split Volume-of-Fluid method generalized for the case where the liquid velocity is not divergence-free and both phases exchange mass across the interface. A sharp interface is maintained by using a Piecewise Linear Interface Construction (PLIC). At supercritical pressures, the dissolution of lighter gas
doi:10.2218/iclass.2021.5914
fatcat:z2ndcl2wa5bcroyb3ssye2n7ea