华南理工大学学报(自然科学版) ›› 2015, Vol. 43 ›› Issue (6): 110-115.doi: 10.3969/j.issn.1000-565X.2015.06.017

• 力学 • 上一篇    下一篇

基于 CEL 算法的水陆两栖飞机水上降落动力特性分析

姚小虎1 黄愉太1 欧智成1 刘晓明2 胡伯仁2   

  1. 1. 华南理工大学 土木与交通学院,广东 广州 510640; 2. 成都飞机工业(集团)有限责任公司 技术中心,四川 成都 610092
  • 收稿日期:2014-05-30 修回日期:2015-01-14 出版日期:2015-06-25 发布日期:2015-05-04
  • 通信作者: 姚小虎(1974-),男,教授,博士生导师,主要从事冲击动力学研究. E-mail:yaoxh@scut.edu.cn
  • 作者简介:姚小虎(1974-),男,教授,博士生导师,主要从事冲击动力学研究.
  • 基金资助:

    国家自然科学基金资助项目(11372113);教育部新世纪优秀人才支持计划项目(NCET-13-0218);华南理工大学中央高校基本科研业务费专项资金资助项目(2014ZG0033)

CEL Algorithm-Based Analysis of Dynamic Characteristics of Amphibious Aircraft Landing on Water

Yao Xiao-hu1 Huang Yu-tai1 Ou Zhi-cheng1 Liu Xiao-ming2 Hu Bo-ren2   

  1. 1. School of Civil Engineering and Transportation,South China University of Technology,Guangzhou 510640,Guangdong,China; 2. Technology Center,Chengdu Aircraft Industrial (Group) Co. ,Ltd. ,Chengdu 610092,Sichuan,China
  • Received:2014-05-30 Revised:2015-01-14 Online:2015-06-25 Published:2015-05-04
  • Contact: 姚小虎(1974-),男,教授,博士生导师,主要从事冲击动力学研究. E-mail:yaoxh@scut.edu.cn
  • About author:姚小虎(1974-),男,教授,博士生导师,主要从事冲击动力学研究.
  • Supported by:
    Supported by the National Natural Science Foundation of China(11372113) and the Program for New Century Excellent Talents in University of Ministry of Education of China(NCET-13-0218)

摘要: 水陆两栖飞机水上降落属于复杂的流固耦合问题,文中建立了某水陆两栖飞机机头的入水流固耦合模型,采用耦合的欧拉 - 拉格朗日(CEL)算法分析了机头入水瞬时的结构动力响应,对比了不同入水角度和不同垂直速度下机头的应力、冲击力及质心速度变化. 结果表明:机头入水初期船底冲击力即出现峰值,之后随着机头抬高,船底冲击力将再次出现峰值;入水过程中机头骨架受力变化明显;随着入水角度的减小,机头应力也减小;入水速度减小,机头应力和船底冲击力都随之减小.

关键词: 水陆两栖飞机, 水上降落, 流固耦合, 动力特性

Abstract: Aiming at the water landing of amphibious aircrafts,this paper presents a fluid-structure interaction (FSI) model of a certain amphibious aircraft head and analyzes the transient structural dynamic response of the head ditching by using the coupled Eulerian-Lagrange (CEL) method. Moreover,the stress,impact force and mass center velocity of the head at different ditching angles and vertical speeds are discussed. The results show that (1) the bottom pressure peak appears in the initial ditching stage and appears again with the heading up of the air-craft head; (2) during the ditching,the pressure of the head skeleton changes significantly; (3) with the de-crease of the hitting angle,the stress of the head reduces; and (4) both the head stress and the bottom impact force reduce with the decrease of ditching speed.

Key words: amphibious aircraft, water landing, fluid-structure interaction, dynamic characteristic