A discrete-adjoint framework for optimizing high-fidelity simulations of turbulent reacting flows

被引:4
|
作者
Kord, Ali [1 ]
Capecelatro, Jesse [1 ,2 ]
机构
[1] Univ Michigan, Dept Mech Engn, Ann Arbor, MI 48109 USA
[2] Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
关键词
Adjoint; Optimization; Combustion; Flamelet; LARGE-EDDY SIMULATION; SENSITIVITY-ANALYSIS; SUMMATION; PARTS; FIELD;
D O I
10.1016/j.proci.2022.06.021
中图分类号
O414.1 [热力学];
学科分类号
摘要
An adjoint-based framework is presented that measures exact sensitivity from high-fidelity simulations of turbulent reacting flows. The framework leverages and extends state-of-the-art numerical methods in a manner that is compatible with a discrete adjoint solver. To ensure energy stability and accuracy, high-order narrow-stencil finite-difference operators satisfying the summation-by-parts (SBP) property are combined with simultaneous-approximation-term boundary treatment. An adaptive SBP dissipation operator and its corresponding adjoint are formulated in a way to dampen unresolved modes and preserve scalar boundedness. A flamelet/progress variable approach is employed to handle chemical reactions using tabulated chemistry. The utility of using pre-computed lookup tables is that discrete adjoint sensitivity can be computed efficiently for arbitrary chemical mechanisms. Gradient-based optimization utilizing the sensitivity obtained from the adjoint solution is demonstrated on two configurations. First, momentum actuation is applied upstream in a spatial mixing layer to control the evolution of a passive scalar in a target region downstream. Then, the framework is used to optimize an acoustic actuator in a three-dimensional turbulent jet with the aim of anchoring an H 2 lifted flame at a target location. Both cases involve manipulating discrete space-time fields with O(10 8 ) - O(10 9 ) degrees of freedom, which would not be possible via a brute-force trial-and-error approach.& COPY; 2022 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
引用
收藏
页码:5375 / 5384
页数:10
相关论文
共 50 条
  • [21] STREAmS: A high-fidelity accelerated solver for direct numerical simulation of compressible turbulent flows
    Bernardini, Matteo
    Modesti, Davide
    Salvadore, Francesco
    Pirozzoli, Sergio
    COMPUTER PHYSICS COMMUNICATIONS, 2021, 263
  • [22] STREAmS: A high-fidelity accelerated solver for direct numerical simulation of compressible turbulent flows
    Bernardini, Matteo
    Modesti, Davide
    Salvadore, Francesco
    Pirozzoli, Sergio
    Computer Physics Communications, 2021, 263
  • [23] Hyperbolic high-fidelity simulations of cratering on a particle bed induced by a turbulent supersonic plume
    Balakrishnan, Kaushik
    Bellan, Josette
    INTERNATIONAL JOURNAL OF MULTIPHASE FLOW, 2024, 179
  • [24] High-Fidelity Simulations of Discrete Roughness Boundary-Layer Transition with Added Perturbations
    Tufts, Matthew W.
    Bisek, Nicholas J.
    Kimmel, Roger L.
    JOURNAL OF SPACECRAFT AND ROCKETS, 2020, 57 (05) : 1079 - 1091
  • [25] Turbulent diffusion of chemically reacting flows: Theory and numerical simulations
    Elperin, T.
    Kleeorin, N.
    Liberman, M.
    Lipatnikov, A. N.
    Rogachevskii, I.
    Yu, R.
    PHYSICAL REVIEW E, 2017, 96 (05)
  • [26] LASER MEASUREMENTS AND STOCHASTIC SIMULATIONS OF TURBULENT REACTING FLOWS.
    Johnston, Sheridan C.
    Dibble, Robert W.
    Schefer, Robert W.
    Ashurst, William T.
    Kollmann, Wolfgang
    AIAA journal, 1986, 24 (06): : 918 - 937
  • [27] HIGH-FIDELITY SIMULATIONS OF IMPINGING JET ATOMIZATION
    Chen, Xiaodong
    Ma, Dongjun
    Yang, Vigor
    Popinet, Stephane
    ATOMIZATION AND SPRAYS, 2013, 23 (12) : 1079 - 1101
  • [28] High-Fidelity Simulations of Rotors in a Compact Configuration
    Miesner, Sebastian
    Kessler, Manuel
    Kraemer, Ewald
    JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 2024, 69 (04)
  • [29] High-fidelity optimization framework for helicopter rotors
    Imiela, Manfred
    AEROSPACE SCIENCE AND TECHNOLOGY, 2012, 23 (01) : 2 - 16
  • [30] High-fidelity Computational Study of High-speed Reacting Jets in Crossflow
    Sharma, Shivank
    Bielawski, Ral
    Rauch, Andreas H.
    Raman, Venkat
    AIAA SCITECH 2024 FORUM, 2024,