NASA Technical Reports Server (NASA) · 1985 · 33 citations · 0 references
Natural SciencesMechanical EngineeringPhysicsAcousticsComputational Fluid DynamicsFluid DynamicsAcoustic ModelingAcoustic Wave PropagationCompressible FlowNumerical AcousticsPressure-velocity CouplingReduced-order ModelingAcoustic Wave EquationsAcoustic WavesDivergenceMach NumberModel Reduction For Fluid DynamicsPressure Fluctuation AnalysisTwo-point Boundary Value ProblemsTwo-point Boundary-value Formulation
This paper concerns a numerical model of a regenerator running at very low temperatures. The model consists of the usual three equations for a compressible fluid with an additional equation for a matrix temperature. The main difficulty with the model is the very low Mach number (approximately 1.E-3). The divergence of the velocity is not small, the pressure divergence is small, and the pressure fluctuation in time is not small. An asymptotic expansion based on the bounded derivative method of Kreiss is used to give a reduced model which eliminates acoustic waves. The velocity is then determined by a two-point boundary value problem which does not contain a time derivative. The solution obtained from the reduced system is compared with the numerical solution of the original system.