Validation of CE/SE Scheme in Low Mach Number Direct Aeroacoustic Simulation
-
Garret C. Y. Lam
,
K. H. Seid
Abstract
The space-time conservation element and solution element (CE/SE) scheme has caught many attention in aeroacoustic research community as an alternative numerical strategy for direct aeroacoustic simulation (DAS). As a result of its strict conversation of flow flux in both space and time, the low-order CE/SE scheme possesses excellent non-dissipative characteristics, expedient in calculating low Mach number DAS which requires uniform numerical accuracy to resolve the widely disparate flow and acoustic scales of the problem. In this paper, an attempt of validating a simplified Courant Number Insensitive CE/SE scheme using carefully selected aeroacoustic benchmark problems is reported. Excellent agreement with the benchmark results obtained firmly establishes that CE/SE scheme is a viable scheme for resolving the nonlinear physics of low Mach number aeroacoustic problems.
©2014 by Walter de Gruyter Berlin/Boston
Articles in the same Issue
- Frontmatter
- Self-excited Oscillations and Fuel Control of a Combustion Process in a Rijke Tube
- Synchronization of Strictly Different Hyperchaotic Systems with Uncertain Parameters and Models
- Modeling of Synthetic Turbulence Generation in Boundary Layer by Using Zonal RANS/LES Method
- A Meshless Method of Lines for Numerical Solution of Some Coupled Nonlinear Evolution Equations
- A Study of Higher Order Terms in Shallow Water Waves via Modified PLK Method
- Numerical Simulation of Stochastic Inverse Problems in Rigid-Poro-Plastic Materials
- Analytic Investigation of a Reaction-diffusion Brusselator Model with the Time-space Fractional Derivative
- Validation of CE/SE Scheme in Low Mach Number Direct Aeroacoustic Simulation
Articles in the same Issue
- Frontmatter
- Self-excited Oscillations and Fuel Control of a Combustion Process in a Rijke Tube
- Synchronization of Strictly Different Hyperchaotic Systems with Uncertain Parameters and Models
- Modeling of Synthetic Turbulence Generation in Boundary Layer by Using Zonal RANS/LES Method
- A Meshless Method of Lines for Numerical Solution of Some Coupled Nonlinear Evolution Equations
- A Study of Higher Order Terms in Shallow Water Waves via Modified PLK Method
- Numerical Simulation of Stochastic Inverse Problems in Rigid-Poro-Plastic Materials
- Analytic Investigation of a Reaction-diffusion Brusselator Model with the Time-space Fractional Derivative
- Validation of CE/SE Scheme in Low Mach Number Direct Aeroacoustic Simulation
