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Ghanshyam Bharate

Publications and source records attributed to Ghanshyam Bharate.

2 recordsLinked to original sources

A Robust All-Mach Six-Equation Diffuse-Interface Method for Multiphase Flows with Surface Tension

A robust finite-volume framework is presented for the simulation of compressible multiphase flows with surface tension across a wide range of Mach numbers. The method is based on a two-pressure, six-equation diffuse interface model incorporating viscous, gravitational, and capillary effects through the continuum surface force formulation. To consistently account for capillary-induced pressure jumps, an HLLC Riemann solver is developed using generalized Riemann invariant analysis, and the instantaneous pressure relaxation procedure is modified to preserve the Laplace pressure jump during phase equilibration. To overcome the excessive numerical diffusion of conventional approximate Riemann solvers in the low-Mach regime, a robust low-Mach correction is proposed by extending our previous formulation with a modified scaling strategy that remains stable in regions of strong pressure variation. The resulting method retains accuracy from nearly incompressible flows to compressible regimes while preserving the robustness of the six-equation formulation. The numerical framework is validated using a series of benchmark problems involving surface tension, viscosity, gravity, and compressibility. The results demonstrate accurate prediction of interface dynamics, capillary pressure, and low-Mach flow features, while significantly reducing numerical dissipation without compromising stability. The proposed methodology provides an efficient and reliable approach for the simulation of complex multiphase flows spanning a broad range of flow regimes.

physics.flu-dyn

Enhanced Diffuse Interface Method for Multiphase Flow Simulations Across All Mach Numbers

This paper enhances the Diffuse Interface Method (DIM) for simulating compressible multiphase flows across all Mach numbers by addressing the accuracy challenges posed at low Mach regimes. A correction to the Riemann solver is introduced, designed to mitigate excessive numerical diffusion while maintaining simplicity and efficiency. The validity of this correction is established through rigorous asymptotic analysis of the governing equations and their discrete counterparts. The proposed correction is implemented within a six-equation model framework with instantaneous relaxation using an HLLC-type solver. Numerical test cases demonstrate significant improvements in accuracy, confirming the effectiveness of the approach in capturing multiphase flow dynamics across a wide range of Mach numbers.

math.NA