• DocumentCode
    175948
  • Title

    Mach number prediction models based on Ensemble Neural Networks for wind tunnel testing

  • Author

    Zhiwei Jin ; Li Zhao ; ZhengZhou Rao

  • Author_Institution
    China Aerodynamics R&D Center, High Speed Aerodynamics Inst., Mianyang, China
  • fYear
    2014
  • fDate
    May 31 2014-June 2 2014
  • Firstpage
    1637
  • Lastpage
    1640
  • Abstract
    The 2.4m×2.4m wind tunnel is a system with the properties of strong nonlinear, multiple variables, serious coupling, large lagging, time-varying, etc. The complexity of all these phenomena makes the development of suitable dynamic Mach number models based on the aerodynamics laws very difficult. As an alternative, the Ensemble Neural Networks (ENN) model based on the feature subsets is proposed to address this problem. ENN built the sub-models on different lower dimension data sets, and reduced the complexity of the single Neural Networks (NN) built on the whole data set. Furthermore, a comparative study among the single NN models and the ENN models when used to predict the Mach number is conducted. Results show that the performance is improved by the ENN models. It is also shows that training time and testing time are much reduced by the ENN models.
  • Keywords
    Mach number; aerodynamics; flow simulation; mechanical engineering computing; mechanical testing; neural nets; wind tunnels; Mach number prediction models; aerodynamics laws; ensemble neural network model; testing time; training time; wind tunnel testing; Aerodynamics; Artificial neural networks; Predictive models; Testing; Training; Wind forecasting; Ensemble Neural Networks; Mach number; Wind tunnel;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control and Decision Conference (2014 CCDC), The 26th Chinese
  • Conference_Location
    Changsha
  • Print_ISBN
    978-1-4799-3707-3
  • Type

    conf

  • DOI
    10.1109/CCDC.2014.6852430
  • Filename
    6852430