摘要
航行体模型试验是获得其流体动力特性的重要手段,针对绕回转体通气空泡模型试验工况多、关键参数影响复杂的问题,通过开展绕回转体通气空泡模型试验的正交设计,减少了模型试验次数,节省试验经费,缩短试验周期,获得影响空泡特征参数的主要因素。研究成果能够指导后续试验研究工作,具有良好的工程应用价值。
Model experiment is an important method of hydrodynamic research.The ventilated cavitation experiment around revolution body always being extensive and complex,orthogonal design of ventilated cavitation experiment can reduce the amount of the cases,save expenditure and shorten the experiment cycle,obtain the main influence factors of the cavity characters based on the results analysis.This work was of a great engineering application value and effective guidance for following study in this field.
出处
《宇航总体技术》
2017年第4期46-51,共6页
Astronautical Systems Engineering Technology
基金
装备发展部共用技术基金(41406040402)
关键词
回转体空化
正交试验
极差分析
方差分析
Revolution body
Cavitation
Orthogonal experiment
Range analysis
Variance analysis
