TY - GEN
T1 - Novel lagrangian-particle tracking method for highly compressible, turbulent, reacting flows
AU - Kozak, Yoram
AU - Dammati, S. Sandeep
AU - Bravo, Luis G.
AU - Hamlington, Peter E.
AU - Poludnenko, Alexei Y.
N1 - Funding Information:
Financial support for this work was provide in part by the Department of Defense High-Performance Computing Modernization Program under the PETTT pre-planned project CFD-KY09-017.
Publisher Copyright:
© 2019 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
Copyright:
Copyright 2020 Elsevier B.V., All rights reserved.
PY - 2019
Y1 - 2019
N2 - In this paper, we discuss a novel Lagrangian-particle tracking method for highly compressible turbulent reacting flows. Both time integration and interpolation schemes are developed with the goal of providing high solution accuracy in the presence of discontinuities in the flow field created by shock waves or flame fronts. It is demonstrated that symplectic time integrators maintain the Lagrangian fluid parcel’s radial position errors low and bounded over the long-time integration periods. While phase errors can grow indefinitely with time, it is shown that they also remain low. Furthermore, it is demonstrated that once discontinuous flow fields are introduced, centered interpolation schemes do not provide adequate accuracy. In order to solve this problem, a new interpolation scheme is developed based on Weighted-Essentially-Non-Oscillatory (WENO) method. When temporal discretization errors are sufficiently small, the new WENO scheme can reduce the trajectory and phase errors by more than an order of magnitude in comparison with the traditional centered schemes. Presented approach can serve as the basis for high-fidelity, efficient numerical particle solvers for direct numerical and large-eddy simulations of high-speed, multiphase, compressible turbulent reacting flows found in hypersonic and detonation-based propulsion systems.
AB - In this paper, we discuss a novel Lagrangian-particle tracking method for highly compressible turbulent reacting flows. Both time integration and interpolation schemes are developed with the goal of providing high solution accuracy in the presence of discontinuities in the flow field created by shock waves or flame fronts. It is demonstrated that symplectic time integrators maintain the Lagrangian fluid parcel’s radial position errors low and bounded over the long-time integration periods. While phase errors can grow indefinitely with time, it is shown that they also remain low. Furthermore, it is demonstrated that once discontinuous flow fields are introduced, centered interpolation schemes do not provide adequate accuracy. In order to solve this problem, a new interpolation scheme is developed based on Weighted-Essentially-Non-Oscillatory (WENO) method. When temporal discretization errors are sufficiently small, the new WENO scheme can reduce the trajectory and phase errors by more than an order of magnitude in comparison with the traditional centered schemes. Presented approach can serve as the basis for high-fidelity, efficient numerical particle solvers for direct numerical and large-eddy simulations of high-speed, multiphase, compressible turbulent reacting flows found in hypersonic and detonation-based propulsion systems.
UR - http://www.scopus.com/inward/record.url?scp=85083944367&partnerID=8YFLogxK
U2 - 10.2514/6.2019-1642
DO - 10.2514/6.2019-1642
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AN - SCOPUS:85083944367
SN - 978-162410578-4
T3 - AIAA Scitech 2019 Forum
BT - AIAA Scitech Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2019
Y2 - 7 January 2019 through 11 January 2019
ER -