导弹与航天运载技术
導彈與航天運載技術
도탄여항천운재기술
MISSILES AND SPACE VEHICLES
2014年
3期
68-70
,共3页
刘晋渤%马爱娥%余亚晖%赵利军
劉晉渤%馬愛娥%餘亞暉%趙利軍
류진발%마애아%여아휘%조리군
变锥度%破片式战斗部%预制破片%飞散特性
變錐度%破片式戰鬥部%預製破片%飛散特性
변추도%파편식전두부%예제파편%비산특성
Variable taper%Fragmentation warhead%Prefabricated fragments%Flight characteristics
针对一种变锥度结构的大型破片式战斗部,采用数值仿真的方法,对战斗部预制破片的飞散速度和飞散角度等特性进行研究,并通过地面静爆试验对仿真计算结果进行验证,结果表明变锥度结构的破片战斗部在增大飞散角方面有明显优势,可有效提高战斗部的杀伤威力。
針對一種變錐度結構的大型破片式戰鬥部,採用數值倣真的方法,對戰鬥部預製破片的飛散速度和飛散角度等特性進行研究,併通過地麵靜爆試驗對倣真計算結果進行驗證,結果錶明變錐度結構的破片戰鬥部在增大飛散角方麵有明顯優勢,可有效提高戰鬥部的殺傷威力。
침대일충변추도결구적대형파편식전두부,채용수치방진적방법,대전두부예제파편적비산속도화비산각도등특성진행연구,병통과지면정폭시험대방진계산결과진행험증,결과표명변추도결구적파편전두부재증대비산각방면유명현우세,가유효제고전두부적살상위력。
A large fragmentation warhead with variable taper structure was investigated, in which the prefabricated fragments flight characteristics such as scatter velocity and scatter angle were numerically simulated. The static-explosion test result agreed with the numerical simulation result. The investigation indicated that the fragmentation warhead with variable taper structure has superiority in increasing the scatter angle, therefore the killing power will be improved obviously.