Test and numerical analysis for water entry of elastic cabin from amphibious aircraft

被引:2
|
作者
Cui, Bo [1 ]
Zhang, Yongjie [1 ]
Dong, Hao [1 ]
Jin, Tao [2 ]
Zhang, Chuzhe [2 ]
Zhu, Qiang [2 ]
机构
[1] Northwestern Polytech Univ, Sch Civil Aviat, Xian 710072, Peoples R China
[2] China Special Vehicle Res Inst, Jingmen 448000, Peoples R China
基金
中国国家自然科学基金;
关键词
Fluid -structure interaction; ALE method; Amphibious aircraft; Water -entry test; Hydroelastic effect; IMPACTS; PANELS; WEDGE;
D O I
10.1016/j.ast.2024.109168
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Water-entry performance of amphibious aircraft is one of the main factors affecting the structural design. However, it is analyzed by rigid models in general, which is difficult to reflect the elastic characteristics of the structure. And it is difficult to obtain sufficient guidance for structural design from rigid-body analysis. In this study, water-entry model of an elastic cabin from amphibious aircraft was developed using the Arbitrary Lagrangian-Eulerian (ALE) method and validated by a designed 1:1 cabin water-entry test. Analysis under various conditions revealed the cabin's dynamic response in three steps: (1) the keel of the cabin section touches the water, (2) the bottom skin is wetted, and (3) the bottom skin is submerged. This study also compares the rigid-surface crashes and water-entry impacts of the cabin from the point of view of load and energy analysis. The results show that rigid-surface crash mainly affects bulkhead and keel, whereas water-entry energy is mainly absorbed by the skin, connectors, and stringers. Additionally, varying skin thicknesses showed a negative correlation with back surface deformation. The methodologies and conclusions presented in this study can offer valuable references for researchers in the field of water entry.
引用
收藏
页数:20
相关论文
共 50 条
  • [41] The Ball-on-Ring-test: Enhancing an analytical solution by numerical analysis for elastic deformation and small displacements
    Staudacher, Maximilian
    Supancic, Peter
    Lube, Tanja
    JOURNAL OF THE EUROPEAN CERAMIC SOCIETY, 2023, 43 (15) : 7167 - 7177
  • [43] Numerical analysis on inlet and outlet sections of a test fuel assembly for a Supercritical Water Reactor
    Kiss, Attila
    Vago, Tamas
    Aszodi, Attila
    NUCLEAR ENGINEERING AND DESIGN, 2015, 295 : 415 - 428
  • [44] Field Test and Numerical Analysis of a New Water-Proof System for a Shield Tunnel
    Zhang Z.
    Xiao S.
    Liu T.
    Huang X.
    He R.
    Shanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong University, 2019, 53 (06): : 688 - 695
  • [45] Numerical Analysis of the Pressure Peak Position Shift With Deadrise Angle in Two-Dimensional Wedge Water Entry
    Zhang, Xu
    Liu, Peiqing
    Qu, Qiulin
    Zhao, Yunke
    Hu, Tianxiang
    Agarwal, Ramesh K.
    JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2018, 140 (11):
  • [46] Methane emissions from a waste treatment site: Numerical analysis of aircraft-based data
    Cai, Yujie
    Cai, Xuhui
    Desjardins, Raymond L.
    Worth, Devon E.
    Srinivasan, Ramesh
    AGRICULTURAL AND FOREST METEOROLOGY, 2020, 292
  • [47] Numerical Analysis and Verification of the Gas Jet from Aircraft Engines Impacting a Jet Blast Deflector
    Fu-Dong Gao
    De-Xin Wang
    Hai-Dong Wang
    Ming-Ming Jia
    Chinese Journal of Mechanical Engineering, 2018, 31
  • [48] Numerical Analysis and Verification of the Gas Jet from Aircraft Engines Impacting a Jet Blast Deflector
    Gao, Fu-Dong
    Wang, De-Xin
    Wang, Hai-Dong
    Jia, Ming-Ming
    CHINESE JOURNAL OF MECHANICAL ENGINEERING, 2018, 31 (01)
  • [49] Numerical Analysis and Verification of the Gas Jet from Aircraft Engines Impacting a Jet Blast Deflector
    Fu-Dong Gao
    De-Xin Wang
    Hai-Dong Wang
    Ming-Ming Jia
    Chinese Journal of Mechanical Engineering, 2018, 31 (05) : 127 - 137
  • [50] Numerical calculation and analysis of infrared radiation characteristics from aircraft skin by using RMC method
    Lv, Jian-Wei
    Wang, Qiang
    Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering, 2009, 38 (02): : 232 - 237