作者: Edoardo Sinibaldi
DOI:
关键词: Flow (mathematics) 、 Riemann problem 、 Finite volume method 、 Liquid-propellant rocket 、 Mathematical optimization 、 Numerical analysis 、 Compressibility 、 Applied mathematics 、 Mathematics 、 Propellant 、 Barotropic fluid
摘要: Starting from a specific industrial problem related to the propellant flow within liquid rocket engine, numerical method for simulating three-dimensional, generic barotropic flows in rotating frames is developed. A novel finite volume compressible approach unstructured grids proposed, suitably preconditioned accurately dealing with nearly-incompressible flows. The time-advancing performed by novel, generic, linearized implicit scheme. constructive procedure solving one-dimensional Riemann associated convex state law presented as well. All proposed ingredients are validated against exact solutions or three-dimensional experimental data complex, also involving cavitation phenomena.