Coupled aerodynamic/structural optimization of a subsonic transport wing using a surrogate model

被引：0
|
作者：
Zhang, Ke-Shi [1 ,2 ]
Han, Zhong-Hua [1 ,2 ]
Li, Wei-Ji [1 ,2 ]
Song, Wen-Ping [1 ,2 ]
机构：
[1] Northwestern Polytechnical University, 710072 Xi'an, China
[2] School of Aeronautics, 127 West Youyi Road, China
来源：
Journal of Aircraft | 1600年 / 45卷 / 06期
关键词：
A multidisciplinary design optimization (MDO) of a high-subsonic transport aircraft wing of a wing/body combination; is demonstrated; which is based on the static aeroelastic effect. A computational method based on quasi-simultaneous viscous-inviscid coupling is used to determine the transonic flow over the wing/body. The structural analysis is carried out by using finite element method (FEM)-based commercial software ANSYS. The surrogate models used for this demonstration improves the computational efficiency and accuracy. Surrogate models like Response-surface method (RSM); kriging model (KM); and radial basis function network (RBF) are used for this optimization. It was observed that surrogate model can easily determine the response due to their low modeling errors. The aeroelastic effect need to be considered to avoid errors in the design phase;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Journal article (JA)
引用
收藏
页码：2167 / 2170
相关论文
共 50 条
  • [1] Coupled Aerodynamic/Structural Optimization of a Subsonic Transport Wing Using a Surrogate Model
    Zhang, Ke-shi
    Han, Zhong-hua
    Li, Wei-ji
    Song, Wen-ping
    JOURNAL OF AIRCRAFT, 2008, 45 (06): : 2167 - 2171
  • [2] Aerostructural Wing Optimization Using a Structural Surrogate in a Coupled Adjoint Formulation
    Fontana, Joshua E.
    Piperni, Pat
    Yang, Zhi
    Mavriplis, Dimitri J.
    AIAA JOURNAL, 2024, 62 (08) : 3093 - 3110
  • [3] A surrogate-based integrated framework for the aerodynamic design optimization of a subsonic wing planform shape
    Benaouali, Abdelkader
    Kachel, Stanislaw
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2018, 232 (05) : 872 - 883
  • [4] Optimization of a Morphing Wing Based on Coupled Aerodynamic and Structural Constraints
    Gamboa, P.
    Vale, J.
    Lau, F. J. P.
    Suleman, A.
    AIAA JOURNAL, 2009, 47 (09) : 2087 - 2104
  • [5] Aerodynamic Shape Optimization Design of the Swept Wing based on the Kriging surrogate model
    Wang, Dan
    Bai, Junqiang
    Hua, Jun
    Sun, Zhiwei
    Qiao, Lei
    ADVANCES IN COMPUTATIONAL MODELING AND SIMULATION, PTS 1 AND 2, 2014, 444-445 : 1277 - +
  • [6] Aerodynamic Optimization Study on Transport Aircraft Wing
    Darshan, Y. N.
    Narahari, H. K.
    Sriram, A. T.
    ADVANCED TRENDS IN MECHANICAL AND AEROSPACE ENGINEERING (ATMA-2019), 2021, 2316
  • [7] Aerodynamic optimization of supersonic transport wing using unstructured adjoint method
    Kim, HJ
    Sasaki, D
    Obayashi, S
    Nakahashi, K
    COMPUTATIONAL FLUID DYNAMICS 2000, 2001, : 581 - 586
  • [8] Aerodynamic optimization of supersonic transport wing using unstructured adjoint method
    Kim, HJ
    Sasaki, D
    Obayashi, S
    Nakahashi, K
    AIAA JOURNAL, 2001, 39 (06) : 1011 - 1020
  • [9] Aerodynamic optimization of supersonic transport wing using unstructured adjoint method
    Kim, H.-J.
    Sasaki, D.
    Obayashi, S.
    Nakahashi, K.
    1600, American Inst. Aeronautics and Astronautics Inc. (39):
  • [10] Aerodynamic and aeroacoustic design optimization of UAVs using a surrogate model
    Sarikaya, Berk
    Zarri, Alessandro
    Christophe, Julien
    Aissa, Mohamed Hassanine
    Verstraete, Tom
    Schram, Christophe
    JOURNAL OF SOUND AND VIBRATION, 2024, 589
12345