摘要
以航弹引信旋翼机构为研究对象 ,着重分析了其在超音速流场中的机构动力特性 ,建立了该机构在超音速条件下的数学模型 .并针对某型旋翼机构进行了计算机仿真 ,为该机构能在超音速条件下继续使用提供了理论参考依据 .
Taking vane actuated mechanism as study object,the paper mainly analyses its dynamic properties in supersonic environment and establishes the mathematical model under this condition.In addition,a computer emulation experiment is made for a certain type of vane driven mechanism.It provides a theoretical and referential basis for its further use in calculating the arming delay in supersonic environmen.
出处
《弹道学报》
CSCD
北大核心
2002年第3期37-41,共5页
Journal of Ballistics
基金
国防科技预研跨行业基金项目
