Structural Optimization and Aeroelastic Analysis of a Subsonic Flying Wing Configuration

被引：0
|
作者：
Li, Liang [1 ]
Sun, Qin [1 ]
机构：
[1] Northwestern Polytech Univ, Xian 710072, Shaanxi, Peoples R China
来源：
PROCEEDINGS OF THE FOURTH INTERNATIONAL CONFERENCE OF MODELLING AND SIMULATION (ICMS2011), VOL 2 | 2011年
关键词：
flying wing; structural optimization; aeroelatic analysis;
D O I：
暂无
中图分类号：
O29 [应用数学];
学科分类号：
070104 ;
摘要：
In this paper, a flying wing model is developed, including structural finite element model and aeroelastic model, and then is made structural optimization and aeroelastic analysis. Throich structural optimization with different constraints and material selections, and aeroelastic analysis, some valued conclusions are achieved, which are useful for future flying wing design.
引用
收藏
页码：155 / 158
页数：4
相关论文
共 50 条
  • [1] An aeroelastic optimization design approach for structural configuration of flying wings
    Yang, C. (yangchao@buaa.edu.cn), 1600, Chinese Society of Astronautics (34):
  • [2] Optimal Structural Topology of a Platelike Wing for Subsonic Aeroelastic Stability
    Stanford, Bret
    Beran, Philip
    JOURNAL OF AIRCRAFT, 2011, 48 (04): : 1193 - 1203
  • [3] Aeroelastic analysis of a wing with freeplay in the subsonic/transonic regions
    Yoo, JH
    Park, YK
    Lee, I
    Han, JH
    JSME INTERNATIONAL JOURNAL SERIES B-FLUIDS AND THERMAL ENGINEERING, 2005, 48 (02) : 208 - 211
  • [4] Airfoil Optimization Design of Flying Wing Configuration
    Li, Long
    Xu, Ying
    Sun, Miao
    Huang, Huang
    Zhang, Ben-Shuang
    2015 INTERNATIONAL CONFERENCE ON MECHANICAL SCIENCE AND MECHANICAL DESIGN, MSMD 2015, 2015, : 418 - 422
  • [5] Buzz aeroelastic responses analysis for a flying wing UAV
    College of Aeronautics, Northwestern Polytechnical University, Xi'an
    710072, China
    不详
    710065, China
    Xibei Gongye Daxue Xuebao, 4 (588-595): : 588 - 595
  • [6] STATIC AEROELASTIC ANALYSIS FOR GENERIC CONFIGURATION WING
    LEE, I
    MIURA, H
    CHARGIN, MK
    JOURNAL OF AIRCRAFT, 1991, 28 (12): : 801 - 802
  • [7] Static aeroelastic analysis for generic configuration wing
    Lee, In
    Miura, Hirokazu
    Chargin, Mladen K.
    1600, (28):
  • [8] Aeroelastic Analysis of High Aspect Ratio Wing in Subsonic Flow
    Ahmad, Kamran
    Wuzhigang
    Rahman, Hammad
    2013 10TH INTERNATIONAL BHURBAN CONFERENCE ON APPLIED SCIENCES AND TECHNOLOGY (IBCAST), 2013, : 219 - 223
  • [9] Effects of structural nonlinearity on subsonic aeroelastic characteristics of an aircraft wing with control surface
    Bae, JS
    Inman, DJ
    Lee, I
    JOURNAL OF FLUIDS AND STRUCTURES, 2004, 19 (06) : 747 - 763
  • [10] Static Aeroelastic Behavior of a Subsonic Plate Wing
    Berci, M.
    PROCEEDINGS OF THE INTERNATIONAL CONFERENCE ON NUMERICAL ANALYSIS AND APPLIED MATHEMATICS 2016 (ICNAAM-2016), 2017, 1863
12345