TY - GEN
T1 - HDMR-based surrogate model for high dimensional aerodynamic design problems
AU - ZhengHong, Gao
AU - Chao, Wang
N1 - Publisher Copyright:
© 2015, American Institute of Aeronautics and Astronautics Inc, AIAA. All rigths reserved.
PY - 2015
Y1 - 2015
N2 - Conventional surrogate models will break down in dealing with high dimensional design problems which is known as the “curse-of-dimensionality”. The purpose of the current work is to develop a more accurate surrogate model for high dimensional problems. In this paper, the High Dimensional Model Representation (HDMR) is studied. The basic idea of HDMR is that for most well-defined physical systems, only relatively low-order correlations of the input variables are expected to have an impact upon the output. The superiority of HDMR-based surrogate model over conventional LHS-based surrogate models is shown through mathematical test functions with a wide scope of dimensionalities. Further, the HDMR-based surrogate model is applied to aerodynamic design of wing with high dimensional design variables. Aerodynamic data of a transonic wing and a supersonic wing are utilized to build the surrogate models and results show that the HDMR-based surrogate model is much better than conventional LHS-based surrogate model.
AB - Conventional surrogate models will break down in dealing with high dimensional design problems which is known as the “curse-of-dimensionality”. The purpose of the current work is to develop a more accurate surrogate model for high dimensional problems. In this paper, the High Dimensional Model Representation (HDMR) is studied. The basic idea of HDMR is that for most well-defined physical systems, only relatively low-order correlations of the input variables are expected to have an impact upon the output. The superiority of HDMR-based surrogate model over conventional LHS-based surrogate models is shown through mathematical test functions with a wide scope of dimensionalities. Further, the HDMR-based surrogate model is applied to aerodynamic design of wing with high dimensional design variables. Aerodynamic data of a transonic wing and a supersonic wing are utilized to build the surrogate models and results show that the HDMR-based surrogate model is much better than conventional LHS-based surrogate model.
UR - http://www.scopus.com/inward/record.url?scp=84960444080&partnerID=8YFLogxK
M3 - 会议稿件
AN - SCOPUS:84960444080
SN - 9781624103681
T3 - 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
BT - 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2015
Y2 - 22 June 2015 through 26 June 2015
ER -