High-Order Finite-Difference Nonlinear Filter Methods for Subsonic Turbulence Simulation with Stochastic ForcingNumerical stability of high-order filter schemes developed by Yee & Sjogreen is tested on three-dimensional turbulence simulations with stochastic forcing and their performance is compared with that of TVD and WENO schemes. The best performing filter method employs an eighth-order central base scheme with the Kennedy & Gruber skew-symmetric splitting of the inviscid flux derivative, a wavelet-based local flow sensor, a nonlinear filter utilizing the dissipative portion of seventh-order \VENO scheme, and an explicit third - or fourth-order Runge-Kutta time integration. We show that the filter scheme is more computational]y efficient and provides a wider spectral bandwidth compared to the seventh-order WENO scheme. The method also demonstrates robust long-time integration for moderately compressible turbulence. In contrast, the fifth- and seventh order WENO schemes show non-trivial evolution of the velocity and density power spectra. over a. few dozen dynamical times, where both TVD and filter schemes recover a so lid statistically stationary turbulent state
Document ID
20190030330
Acquisition Source
Ames Research Center
Document Type
Abstract
Authors
Kritsuk, Alexei G. (California Univ. San Diego, CA, United States)
Kotov, Dmitry (NASA Ames Research Center Moffett Field, CA, United States)
Sjogreen, Bjorn (Lawrence Livermore National Lab. Livermore, CA, United States)
Yee, Helen C. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2019
Publication Date
July 1, 2019
Subject Category
Mathematical And Computer Sciences (General)Aeronautics (General)