TY - GEN
T1 - Shape Recognition of Fuel Atomization in Crossflow using Deep Learning
AU - Sakano, Yukari
AU - Sato, Tetsuya
AU - Nambu, Taisuke
AU - Mizobuchi, Yasuhiro
N1 - Funding Information:
Calculation in this paper was performed on JAXA Super-computer System generation 2 (JSS2) and JAXA Supercomputer System generation 3 (JSS3). Furthermore, I wish to express my gratitude to numerical simulation research unit in JAXA Aeronautical Technology Directorate for helpful suggestions.
Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2022
Y1 - 2022
N2 - To design aerospace engines efficiently, it is important to develop numerical analysis models of atomization. However, crossflow atomization, which is applied in engines that use a premixing/pre-vaporizing lean combustion in main burner, creates very complicated fluid structures and a general model for its analysis has yet to be developed. To analyze this phenomenon, it is important to consider the difference in the required resolutions between the gas field and atomized droplets, and Euler-Lagrange coupling analysis has been proposed to address this. However, in previous studies, only sufficiently spherical droplets could be replaced by Lagrange particles, and this reduces accuracy. We therefore propose a secondary atomization model that considers droplet shape and increases the number of droplets which can be replaced. To reduce the computational cost of analyzing three-dimensional droplet shape data, we applied deep learning to droplet shape recognition and breakup behavior prediction. As a result of this shape consideration, the accuracy of predicting whether or not a droplet exhibits “breakup” increased from 65.60 % to 77.68 % compared to a prediction using the theory of previous substantial model that treats all droplets as spheres. In addition, deep learning reduced the droplet shape recognition time from 4.90 s to 0.21 s compared to a method based on geometric parameters.
AB - To design aerospace engines efficiently, it is important to develop numerical analysis models of atomization. However, crossflow atomization, which is applied in engines that use a premixing/pre-vaporizing lean combustion in main burner, creates very complicated fluid structures and a general model for its analysis has yet to be developed. To analyze this phenomenon, it is important to consider the difference in the required resolutions between the gas field and atomized droplets, and Euler-Lagrange coupling analysis has been proposed to address this. However, in previous studies, only sufficiently spherical droplets could be replaced by Lagrange particles, and this reduces accuracy. We therefore propose a secondary atomization model that considers droplet shape and increases the number of droplets which can be replaced. To reduce the computational cost of analyzing three-dimensional droplet shape data, we applied deep learning to droplet shape recognition and breakup behavior prediction. As a result of this shape consideration, the accuracy of predicting whether or not a droplet exhibits “breakup” increased from 65.60 % to 77.68 % compared to a prediction using the theory of previous substantial model that treats all droplets as spheres. In addition, deep learning reduced the droplet shape recognition time from 4.90 s to 0.21 s compared to a method based on geometric parameters.
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U2 - 10.2514/6.2022-0227
DO - 10.2514/6.2022-0227
M3 - Conference contribution
AN - SCOPUS:85122654853
SN - 9781624106316
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
SP - 1
EP - 18
BT - AIAA SciTech Forum 2022
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Y2 - 3 January 2022 through 7 January 2022
ER -