TY - JOUR
T1 - Explicit discontinuous spectral element method with entropy generation based artificial viscosity for shocked viscous flows
AU - Chaudhuri, A.
AU - Jacobs, G. B.
AU - Don, W. S.
AU - Abbassi, H.
AU - Mashayek, F.
N1 - The authors gratefully acknowledge the financial support from the Office of the Secretary of Defense (FA8650-12-C-2247). The authors are also grateful to the Air Force Research laboratory (AFRL) for managing the project. The third author thanks the Ocean University of China for providing the research fund (201412003) used in this work. We would like to thank Prof. S. Pirozzoli (Sapienza University of Rome) for providing the DNS database used for 3D turbulent inflow generation. Also, we express our gratitude to Prof. E.T. Van Der Weide (University of Twente) for providing the Matlab routine to generate exact NS solution of viscous shock structure.
Publisher Copyright:
© 2016 Elsevier Inc.
PY - 2017/3/1
Y1 - 2017/3/1
N2 - A spatio-temporal adaptive artificial viscosity (AV) based shock-capturing scheme is proposed for the solution of both inviscid and viscous compressible flows using a high-order parallel Discontinuous Spectral Element Method (DSEM). The artificial viscosity and artificial thermal conduction coefficients are proportional to the viscous and thermal entropy generating terms, respectively, in the viscous entropy conservation law. The magnitude of AV is limited based on the explicit stable CFL criterion, so that the stable artificial viscous time step size is greater than the convective stable time step size. To further ensure the stability of this explicit approach, an adaptive variable order exponential filter is applied, if necessary, in elements where the AV has been limited. In viscous flow computations a modified Jameson's sensor (Ducros et al., 1999 [61]) limits the AV to small values in viscous shear regions, so as to maintain a high-order resolution in smooth regions and an essentially non-oscillatory behavior near sharp gradients/shocks regions. We have performed a systematic and extensive validation of the algorithm with one-dimensional problems (inviscid moving shock and viscous shock-structure interaction), two-dimensional problems (inviscid steady and unsteady shocked flows and viscous shock-boundary layer interaction), and a three-dimensional supersonic turbulent flow over a ramped cavity. These examples demonstrate that the explicit DSEM scheme with adaptive artificial viscosity terms is stable, accurate and efficient.
AB - A spatio-temporal adaptive artificial viscosity (AV) based shock-capturing scheme is proposed for the solution of both inviscid and viscous compressible flows using a high-order parallel Discontinuous Spectral Element Method (DSEM). The artificial viscosity and artificial thermal conduction coefficients are proportional to the viscous and thermal entropy generating terms, respectively, in the viscous entropy conservation law. The magnitude of AV is limited based on the explicit stable CFL criterion, so that the stable artificial viscous time step size is greater than the convective stable time step size. To further ensure the stability of this explicit approach, an adaptive variable order exponential filter is applied, if necessary, in elements where the AV has been limited. In viscous flow computations a modified Jameson's sensor (Ducros et al., 1999 [61]) limits the AV to small values in viscous shear regions, so as to maintain a high-order resolution in smooth regions and an essentially non-oscillatory behavior near sharp gradients/shocks regions. We have performed a systematic and extensive validation of the algorithm with one-dimensional problems (inviscid moving shock and viscous shock-structure interaction), two-dimensional problems (inviscid steady and unsteady shocked flows and viscous shock-boundary layer interaction), and a three-dimensional supersonic turbulent flow over a ramped cavity. These examples demonstrate that the explicit DSEM scheme with adaptive artificial viscosity terms is stable, accurate and efficient.
KW - Adaptive filter
KW - Artificial viscosity
KW - Discontinuous spectral element
KW - Shock sensor
KW - Supersonic cavity flow
KW - Viscous compressible flows
UR - https://www.scopus.com/pages/publications/85006100709
U2 - 10.1016/j.jcp.2016.11.042
DO - 10.1016/j.jcp.2016.11.042
M3 - Journal article
AN - SCOPUS:85006100709
SN - 0021-9991
VL - 332
SP - 99
EP - 117
JO - Journal of Computational Physics
JF - Journal of Computational Physics
ER -