Fast and reliable prediction of scramjet flowfields via Gaussian process latent variable model and deep learning

被引:15
作者
Fujio, Chihiro [1 ]
Akiyama, Kento [1 ]
Ogawa, Hideaki [1 ]
机构
[1] Kyushu Univ, Dept Aeronaut & Astronaut, 744 Motooka,Nishi Ku, Fukuoka, Fukuoka 8190395, Japan
基金
日本科学技术振兴机构; 日本学术振兴会;
关键词
DESIGN OPTIMIZATION; PHYSICAL INSIGHT;
D O I
10.1063/5.0148974
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Fast and accurate prediction of high-speed flowfields is of particular interest to researchers in fluid science and engineering to enable efficient design exploration and knowledge discovery. The reliability of prediction is another important metric for the performance of prediction models. While predictive modeling approaches with and without reduced-order modeling (ROM) via machine learning techniques have been proposed, they are inherently subject to loss of information for ROM-based approaches and substantial computational costs in modeling for non-ROM-based approaches. This paper proposes an accurate ROM-based predictive framework with minimum information loss enabled by incorporating Gaussian process latent variable modeling (GPLVM) and deep learning. The stochastic nature of GPLVM allows for uncertainty quantification that indicates the degree of prediction error or reliability of prediction without requiring validation data. The applicability for supersonic/hypersonic viscous flowfields has been examined for two cases including axisymmetric intakes and two-dimensional fuel injection in scramjet engines by comparison with other predictive models. Comparable or superior prediction accuracy over the other models has been achieved by the proposed approaches, demonstrating its high potential to serve as a new competent, data-driven technique for fast, accurate, and reliable prediction of scramjet flowfields.
引用
收藏
页数:19
相关论文
共 49 条
  • [21] Optimization design of energy deposition on single expansion ramp nozzle
    Ju, Shengjun
    Yan, Chao
    Wang, Xiaoyong
    Qin, Yupei
    Ye, Zhifei
    [J]. ACTA ASTRONAUTICA, 2017, 140 : 351 - 361
  • [22] Kingma Diederik P., 2015, ICLR POSTER
  • [23] A deep learning approach for the velocity field prediction in a scramjet isolator
    Kong, Chen
    Chang, Juntao
    Li, Yunfei
    Wang, Ziao
    [J]. PHYSICS OF FLUIDS, 2021, 33 (02)
  • [24] Application of CFD and the Kriging method for optimizing the performance of a generic scramjet combustor
    Kumar, Sudarshan
    Das, Sudipto
    Sheelam, Shekher
    [J]. ACTA ASTRONAUTICA, 2014, 101 : 111 - 119
  • [25] Lawrence N, 2005, J MACH LEARN RES, V6, P1783
  • [26] Recent progress of machine learning in flow modeling and active flow control
    Li, Yunfei
    Chang, Juntao
    Kong, Chen
    Bao, Wen
    [J]. CHINESE JOURNAL OF AERONAUTICS, 2022, 35 (04) : 14 - 44
  • [27] An efficient deep learning framework to reconstruct the flow field sequences of the supersonic cascade channel
    Li, Yunfei
    Chang, Juntao
    Wang, Ziao
    Kong, Chen
    [J]. PHYSICS OF FLUIDS, 2021, 33 (05)
  • [28] ON THE LIMITED MEMORY BFGS METHOD FOR LARGE-SCALE OPTIMIZATION
    LIU, DC
    NOCEDAL, J
    [J]. MATHEMATICAL PROGRAMMING, 1989, 45 (03) : 503 - 528
  • [29] Lumley J.L., 1967, ATMOSPHERIC TURBULEN, P166
  • [30] 2-EQUATION EDDY-VISCOSITY TURBULENCE MODELS FOR ENGINEERING APPLICATIONS
    MENTER, FR
    [J]. AIAA JOURNAL, 1994, 32 (08) : 1598 - 1605