A discrete-adjoint framework for optimizing high-fidelity simulations of turbulent reacting flows
被引:4
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作者:
Kord, Ali
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Univ Michigan, Dept Mech Engn, Ann Arbor, MI 48109 USAUniv Michigan, Dept Mech Engn, Ann Arbor, MI 48109 USA
Kord, Ali
[1
]
Capecelatro, Jesse
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Univ Michigan, Dept Mech Engn, Ann Arbor, MI 48109 USA
Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USAUniv Michigan, Dept Mech Engn, Ann Arbor, MI 48109 USA
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
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.
机构:
Dipartimento di Ingegneria Meccanica e Aerospaziale, Sapienza Università di Roma, via Eudossiana 18, Roma,00184, ItalyDipartimento di Ingegneria Meccanica e Aerospaziale, Sapienza Università di Roma, via Eudossiana 18, Roma,00184, Italy
Bernardini, Matteo
Modesti, Davide
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机构:
Aerodynamics Group, Faculty of Aerospace Engineering, Delft University of Technology, Kluyverweg 2, Delft,2629 HS, NetherlandsDipartimento di Ingegneria Meccanica e Aerospaziale, Sapienza Università di Roma, via Eudossiana 18, Roma,00184, Italy
Modesti, Davide
Salvadore, Francesco
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机构:
HPC Department, CINECA, Rome office, via dei Tizii 6/B, Roma,00185, ItalyDipartimento di Ingegneria Meccanica e Aerospaziale, Sapienza Università di Roma, via Eudossiana 18, Roma,00184, Italy
Salvadore, Francesco
Pirozzoli, Sergio
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Dipartimento di Ingegneria Meccanica e Aerospaziale, Sapienza Università di Roma, via Eudossiana 18, Roma,00184, ItalyDipartimento di Ingegneria Meccanica e Aerospaziale, Sapienza Università di Roma, via Eudossiana 18, Roma,00184, Italy
机构:
CALTECH, Jet Prop Lab, 4800 Oak Grove Dr, Pasadena, CA 91109 USACALTECH, Jet Prop Lab, 4800 Oak Grove Dr, Pasadena, CA 91109 USA
Balakrishnan, Kaushik
Bellan, Josette
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机构:
CALTECH, Jet Prop Lab, 4800 Oak Grove Dr, Pasadena, CA 91109 USA
CALTECH, Pasadena, CA 91125 USACALTECH, Jet Prop Lab, 4800 Oak Grove Dr, Pasadena, CA 91109 USA
机构:
US Air Force, Res Lab, Aerosp Syst Directorate, Wright Patterson AFB, OH 45433 USAUS Air Force, Res Lab, Aerosp Syst Directorate, Wright Patterson AFB, OH 45433 USA
Tufts, Matthew W.
Bisek, Nicholas J.
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机构:
US Air Force, Res Lab, Aerosp Syst Directorate, Wright Patterson AFB, OH 45433 USAUS Air Force, Res Lab, Aerosp Syst Directorate, Wright Patterson AFB, OH 45433 USA
Bisek, Nicholas J.
Kimmel, Roger L.
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US Air Force, Res Lab, Aerosp Syst Directorate, Wright Patterson AFB, OH 45433 USAUS Air Force, Res Lab, Aerosp Syst Directorate, Wright Patterson AFB, OH 45433 USA
机构:
Ben Gurion Univ Negev, Dept Mech Engn, Pearlstone Ctr Aeronaut Engn Studies, POB 653, IL-84105 Beer Sheva, IsraelBen Gurion Univ Negev, Dept Mech Engn, Pearlstone Ctr Aeronaut Engn Studies, POB 653, IL-84105 Beer Sheva, Israel
Elperin, T.
Kleeorin, N.
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机构:
Ben Gurion Univ Negev, Dept Mech Engn, Pearlstone Ctr Aeronaut Engn Studies, POB 653, IL-84105 Beer Sheva, IsraelBen Gurion Univ Negev, Dept Mech Engn, Pearlstone Ctr Aeronaut Engn Studies, POB 653, IL-84105 Beer Sheva, Israel
Kleeorin, N.
Liberman, M.
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机构:
KTH Royal Inst Technol, NORDITA, Roslagstullsbacken 23, S-10691 Stockholm, Sweden
Stockholm Univ, Roslagstullsbacken 23, S-10691 Stockholm, SwedenBen Gurion Univ Negev, Dept Mech Engn, Pearlstone Ctr Aeronaut Engn Studies, POB 653, IL-84105 Beer Sheva, Israel
机构:
Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USAUniv Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
Sharma, Shivank
Bielawski, Ral
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机构:
Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USAUniv Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
Bielawski, Ral
Rauch, Andreas H.
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机构:
Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
Univ Michigan, Michigan Inst Data Sci, Ann Arbor, MI 48109 USAUniv Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
Rauch, Andreas H.
Raman, Venkat
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机构:
Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USAUniv Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA