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
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