摘要
小攻角下水下航行体高速运动时会形成不对称、非定常空泡,空泡形态是水下流体动力及弹道设计的主要依据。该文基于空泡独立膨胀原理,考虑横流对独立空泡发展的影响,建立了带攻角状态下空泡形态理论计算模型。针对典型工况开展计算获得了航行体迎背流面空泡长度、空泡压力变化过程,并与试验数据进行比对以验证模型的合理性。
Asymmetry of unsteady cavities can be formed when the body moves with a＇ high speed and small attack angle, which is the main design basis of hydrodynamics and hydroballistics. Theoretical model is es- tablished based on Logvinovich independence principle, considering the influence of crossflow effect. A typi- cal case is simulated to get cavity length of the face flow surface and the back flow surface, as well as cavity pressure. Finally, the comparison is performed between the results of the theoretical model and the experi- ment, which confirms the theoretical approach in this study.
出处
《船舶力学》
EI
CSCD
北大核心
2015年第8期889-895,共7页
Journal of Ship Mechanics
基金
国防基础科研项目(A0320110015)
973项目(613171)
关键词
空泡形态
局部空化
独立膨胀原理
流体动力
非定常
cavity shape
partially cavitation
Logvinovich independence principle
hydrodynamics
unsteady
