TY - GEN
T1 - A novel surrogate model for emulation of bi-fluid swirl injector flow dynamics
AU - Li, Yixing
AU - Wang, Xingjian
AU - Chang, Yu Hung
AU - Milan, Petro Junior
AU - Yang, Vigor
N1 - Publisher Copyright:
© 2020 American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2020
Y1 - 2020
N2 - The present study proposes and implements a high-fidelity data-driven emulation framework to predict spatiotemporal flow field in gas-centered, liquid-swirl coaxial (GCLSC) injectors, operating at supercritical conditions. In this injector, the mixing process of high-speed gaseous oxygen and swirling kerosene renders complicated flow dynamics. The emulation framework employs the common kernel-smoothed proper orthogonal decomposition (CKSPOD) technique as the surrogate model. The CKSPOD technique extracts dominant coherent flow structures through Hadamard-based POD, conducts kriging-based training process, and then reconstructs the structures to predict the flowfield of a new case. Significant improvements, including common-grid interpolation and physics-based conditions, are incorporated to the current framework to accommodate the prediction of complicated flow dynamics and mixing characteristics with varying geometry. In this study, recess length is chosen as the varying design parameter, and the LES results of GCLSC injectors at all design settings are collected to train the CKSPOD-based emulator. Detailed evaluations of the predicted flow fields are carried out, and the current framework can capture spatiotemporally evolving flow field, as well as propellant mixing with high accuracy. Good agreements are also achieved for time-averaged flow fields. In addition to the highly accurately prediction, the developed framework significantly reduces the computational time for the evaluation of new injector designs and will serve as a competitive tool for efficient survey of the design space.
AB - The present study proposes and implements a high-fidelity data-driven emulation framework to predict spatiotemporal flow field in gas-centered, liquid-swirl coaxial (GCLSC) injectors, operating at supercritical conditions. In this injector, the mixing process of high-speed gaseous oxygen and swirling kerosene renders complicated flow dynamics. The emulation framework employs the common kernel-smoothed proper orthogonal decomposition (CKSPOD) technique as the surrogate model. The CKSPOD technique extracts dominant coherent flow structures through Hadamard-based POD, conducts kriging-based training process, and then reconstructs the structures to predict the flowfield of a new case. Significant improvements, including common-grid interpolation and physics-based conditions, are incorporated to the current framework to accommodate the prediction of complicated flow dynamics and mixing characteristics with varying geometry. In this study, recess length is chosen as the varying design parameter, and the LES results of GCLSC injectors at all design settings are collected to train the CKSPOD-based emulator. Detailed evaluations of the predicted flow fields are carried out, and the current framework can capture spatiotemporally evolving flow field, as well as propellant mixing with high accuracy. Good agreements are also achieved for time-averaged flow fields. In addition to the highly accurately prediction, the developed framework significantly reduces the computational time for the evaluation of new injector designs and will serve as a competitive tool for efficient survey of the design space.
UR - http://www.scopus.com/inward/record.url?scp=85091740270&partnerID=8YFLogxK
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U2 - 10.2514/6.2020-1070
DO - 10.2514/6.2020-1070
M3 - Conference contribution
AN - SCOPUS:85091740270
SN - 9781624105951
T3 - AIAA Scitech 2020 Forum
SP - 1
EP - 32
BT - AIAA Scitech 2020 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2020
Y2 - 6 January 2020 through 10 January 2020
ER -