一种机动飞行条件下的飞机整体油箱流固耦合分析方法
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  • 英文篇名:Fluid Solid Coupling Analysis of Integral Fuel Tank in Maneuvering Flight State
  • 作者:赖辉 ; 陈晓峰 ; 刘海 ; 赵博伟
  • 英文作者:LAI Hui;CHEN Xiaofeng;LIU Hai;ZHAO Bowei;Technology Center,AVIC Chengdu Aircraft Industrial(Group) Co.,Ltd.;
  • 关键词:整体油箱 ; 流固耦合 ; 机动飞行 ; ABAQUS ; STAR-CCM+
  • 英文关键词:integral fuel tank;;fluid solid coupling;;maneuvering flight;;ABAQUS;;STAR-CCM+
  • 中文刊名:CDDD
  • 英文刊名:Journal of Chengdu University(Natural Science Edition)
  • 机构:航空工业成都飞机工业(集团)有限责任公司技术中心;
  • 出版日期:2019-03-30
  • 出版单位:成都大学学报(自然科学版)
  • 年:2019
  • 期:v.38;No.129
  • 语种:中文;
  • 页:CDDD201901020
  • 页数:5
  • CN:01
  • ISSN:51-1216/N
  • 分类号:90-94
摘要
为了校核飞机机动飞行条件下整体油箱的结构强度以及密封性能,基于ABAQUS和STAR-CCM+仿真分析工具,探索了一种机动飞行条件下的飞机整体油箱流固耦合数值仿真分析方法,完成了某型飞机机身整体油箱的流固耦合分析,并采用SPH方法对比验证了仿真分析计算结果的准确性.
        In order to check both the structural strength and the sealing property of the integral fuel tank in maneuvering flight state,based on commercial software ABAQUS and STARCCM+,the paper explored a fluid solid coupling simulation method of integral fuel tank in maneuvering flight state,and accomplished the fluid solid coupling simulation of the integral fuel tank.The SPH method was used to verify the simulation results of our study.
引文
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