4.7 Article

A hybrid numerical simulation of isotropic compressible turbulence

Journal

JOURNAL OF COMPUTATIONAL PHYSICS
Volume 229, Issue 13, Pages 5257-5279

Publisher

ACADEMIC PRESS INC ELSEVIER SCIENCE
DOI: 10.1016/j.jcp.2010.03.042

Keywords

Compressible turbulence; Compact finite difference; WENO; Hybrid approach; Shocklets

Funding

  1. National Natural Science Foundation of China [NSFC-10921202]
  2. Ministry of Science and Technology of China [2009CB724101]
  3. US National Science Foundation [ATM-0527140, ATM-0730766, OCI-0904534]
  4. College of Engineering of Peking University in China
  5. College of Engineering of the University of Delaware
  6. US National Center for Atmospheric Research [CISL-35751010, CISL-35751014]
  7. Directorate For Geosciences
  8. Div Atmospheric & Geospace Sciences [0730766] Funding Source: National Science Foundation

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A novel hybrid numerical scheme with built-in hyperviscosity has been developed to address the accuracy and numerical instability in numerical simulation of isotropic compressible turbulence in a periodic domain at high turbulent Mach number. The hybrid scheme utilizes a 7th-order WENO (Weighted Essentially Non-Oscillatory) scheme for highly compressive regions (i.e., shocklet regions) and an 8th-order compact central finite difference scheme for smooth regions outside shocklets. A flux-based conservative and formally consistent formulation is developed to optimize the connection between the two schemes at the interface and to achieve a higher computational efficiency. In addition, a novel numerical hyperviscosity formulation is proposed within the context of compact finite difference scheme for the smooth regions to improve numerical stability of the hybrid method. A thorough and insightful analysis of the hyperviscosity formulation in both Fourier space and physical space is presented to show the effectiveness of the formulation in improving numerical stability, without compromising the accuracy of the hybrid method. A conservative implementation of the hyperviscosity formulation is also developed. Combining the analysis and test simulations, we have also developed a criterion to guide the specification of a numerical hyperviscosity coefficient (the only adjustable coefficient in the formulation). A series of test simulations are used to demonstrate the accuracy and numerical stability of the scheme for both decaying and forced compressible turbulence. Preliminary results for a high-resolution simulation at turbulent Mach number of 1.08 are shown. The sensitivity of the simulated flow to the detail of thermal forcing method is also briefly discussed. (c) 2010 Elsevier Inc. All rights reserved.

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