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气缸张开式尾翼的测试与计算
引用本文:汪东晖,赵有守,王儒策.气缸张开式尾翼的测试与计算[J].南京理工大学学报(自然科学版),1989(3).
作者姓名:汪东晖  赵有守  王儒策
作者单位:机械工程二系 (汪东晖,赵有守),机械工程二系(王儒策)
摘    要:本文对某破甲弹用高速摄影仪拍摄尾翼张开过程的振动,压力测试系统测量气缸室内的模拟压力曲线,并对气缸内p-t曲线进行理论计算.为研究气缸张开式尾翼张开过程的振动,防止引信炮口早炸提供测试方法与计算.

关 键 词:破甲弹[75D]  冲击力[31BC]  引信安全性[75J]  实验[92F]  张开式尾翼

Measurement and Calculation of Cylinder-Open Fin.
Wang Donghui,Zhao Youshou,Wang Ruche.Measurement and Calculation of Cylinder-Open Fin.[J].Journal of Nanjing University of Science and Technology(Nature Science),1989(3).
Authors:Wang Donghui  Zhao Youshou  Wang Ruche
Institution:Wang Donghui;Zhao Youshou;Wang Ruche
Abstract:In this paper, high--speed photograph was madeof high erplosive anti-tank projectile to study it s fin op-ening, the simulated pressure curve within the cylinder was me-asured by pressure-testing system, and theoretical calculation ofp-t curve of the cylinder was carried out. A test method andcalculation were presented for studying vibration during fin's op-ening and preventing the early burst of fuze near the nozzle.
Keywords:High explosive anti-tank cartridge  Impulsive force  Fuze safety  Experiments  Cylinder-open fin  
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