• DocumentCode
    3072242
  • Title

    Simulation of Tail-slap Loads of Supercavitating Projectiles

  • Author

    Zhang, Jia-Zhong ; Zhang, Jin-Sheng ; Wei, Ying-Jie

  • Author_Institution
    Sch. of Astronaut., Harbin Inst. of Technol., Harbin, China
  • Volume
    2
  • fYear
    2010
  • fDate
    4-6 June 2010
  • Firstpage
    163
  • Lastpage
    166
  • Abstract
    To investigate the tail-slap loads on supercavitating projectiles, a simple model for cavity-fluid region is presented based on Logvinovich´s Principle. And a series of simulations of fluid - structure interaction (FSI) were done to determine the effects of the slenderness ratio of projectiles on the tail-slap loads. The results show that the impact duration increases as the slenderness ratio increases and the frequency of impacts decrease as the slenderness ratio increases. The larger the slenderness ratio is, the more obviously the body´s flexibility and vibration influent the slapping force. The results developed in this paper will provide reference for the structural dynamics research and optimization design of the supercavitating projectiles.
  • Keywords
    cavitation; impact (mechanical); projectiles; structural engineering; vibrations; cavity-fluid region; fluid-structure interaction simulation; impacts; projectiles; slapping force; structural dynamics; supercavitation; tail-slap loads; vibration; Analytical models; Computational modeling; Drag; Electronic mail; Fluid dynamics; Frequency; Projectiles; Sensor phenomena and characterization; Space technology; Tail; FSI; impact load; numerical simulation; supercavity; tail slap;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Information and Computing (ICIC), 2010 Third International Conference on
  • Conference_Location
    Wuxi, Jiang Su
  • Print_ISBN
    978-1-4244-7081-5
  • Electronic_ISBN
    978-1-4244-7082-2
  • Type

    conf

  • DOI
    10.1109/ICIC.2010.135
  • Filename
    5513880