Generative adversarial networks with physical evaluators for spray simulation of pintle injector

被引:6
|
作者
Ma, Hao [1 ]
Zhang, Botao [2 ]
Zhang, Chi [3 ]
Haidn, Oskar J. [1 ]
机构
[1] Tech Univ Munich, Dept Aerosp & Geodesy, D-85748 Garching, Germany
[2] Xian Aerosp Prop Inst, Key Lab Liquid Rocket Engine Technol, Xian 710100, Peoples R China
[3] Tech Univ Munich, Dept Mech Engn, D-85748 Garching, Germany
关键词
COMBUSTION CHARACTERISTICS; NEURAL-NETWORKS; ROCKET;
D O I
10.1063/5.0056549
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
Due to the adjustable geometry, pintle injectors are especially suitable for liquid rocket engines, which require a widely throttleable range. However, applying the conventional computational fluid dynamics approaches to simulate the complex spray phenomenon in the whole range still remains a great challenge. In this paper, a novel deep learning approach used to simulate instantaneous spray fields under continuous operating conditions is explored. Based on one specific type of neural network and the idea of physics constraint, a Generative Adversarial Networks with Physics Evaluators framework is proposed. The geometry design and mass flux information are embedded as inputs. After the adversarial training between the generator and discriminator, the generated field solutions are fed into two physics evaluators. In this framework, a mass conversation evaluator is designed to improve the training robustness and convergence. A spray angle evaluator, which is composed of a down-sampling Convolutional Neural Network and theoretical model, guides the networks to generate the spray solutions more closely according to the injection conditions. The characterization of the simulated spray, including the spray morphology, droplet distribution, and spray angle, is well predicted. This work suggests great potential for prior physics knowledge employment in the simulation of instantaneous flow fields. (c) 2021 Author(s).
引用
收藏
页数:11
相关论文
共 50 条
  • [1] Verification on Spray Simulation of a Pintle Injector for Liquid Rocket Engine
    Son, Min
    Yu, Kijeong
    Radhakrishnan, Kanmaniraja
    Shin, Bongchul
    Koo, Jaye
    JOURNAL OF THERMAL SCIENCE, 2016, 25 (01) : 90 - 96
  • [2] Verification on Spray Simulation of a Pintle Injector for Liquid Rocket Engine
    Min Son
    Kijeong Yu
    Kanmaniraja Radhakrishnan
    Bongchul Shin
    Jaye Koo
    Journal of Thermal Science, 2016, 25 (01) : 90 - 96
  • [3] Verification on spray simulation of a pintle injector for liquid rocket engine
    Min Son
    Kijeong Yu
    Kanmaniraja Radhakrishnan
    Bongchul Shin
    Jaye Koo
    Journal of Thermal Science, 2016, 25 : 90 - 96
  • [4] Spray Characteristics of a Movable Pintle Injector with Pintle Tip Shape
    Nam, Jeongsoo
    Lee, Keonwoong
    Park, Sunjung
    Huh, Hwanil
    Koo, Jaye
    JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2019, 47 (09) : 658 - 664
  • [5] Experimental research on the spray characteristics of pintle injector
    Chen, Huiyuan
    Li, Qinglian
    Cheng, Peng
    ACTA ASTRONAUTICA, 2019, 162 : 424 - 435
  • [6] LAGRANGIAN APPROACH TO AXISYMMETRIC SPRAY SIMULATION OF PINTLE INJECTOR FOR LIQUID ROCKET ENGINES
    Radhakrishnan, Kanmaniraja
    Son, Min
    Lee, Keonwoong
    Koo, Jaye
    ATOMIZATION AND SPRAYS, 2018, 28 (05) : 443 - 458
  • [7] Analysis on spray angle model for pintle injector element
    Wang K.
    Lei F.
    Zhang B.
    Yang A.
    Zhou L.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2020, 41 (10):
  • [8] Generative Adversarial Networks for fast simulation
    Carminati, Federico
    Khattak, Gulrukh
    Loncar, Vladimir
    Nguyen, Thong Q.
    Pierini, Maurizio
    Da Rocha, Ricardo Brito
    Samaras-Tsakiris, Konstantinos
    Vallecorsa, Sofia
    Vlimant, Jean-Roch
    19TH INTERNATIONAL WORKSHOP ON ADVANCED COMPUTING AND ANALYSIS TECHNIQUES IN PHYSICS RESEARCH, 2020, 1525
  • [9] Research Progress on Spray Combustion Characteristics of Pintle Injector
    Xie Y.
    Nie W.-S.
    Jiang C.-J.
    Luo X.-Q.
    Tong Y.-H.
    Tuijin Jishu/Journal of Propulsion Technology, 2022, 43 (07):
  • [10] Effects of skip distance on the spray characteristics of a pintle injector
    Lee, Suji
    Koo, Jaye
    Yoon, Youngbin
    ACTA ASTRONAUTICA, 2021, 178 : 471 - 480