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
Link To Document