含能材料
含能材料
함능재료
ENERGETIC MATERIALS
2013年
5期
656-659
,共4页
杨桂红%王广军%龚晏青%孙永强
楊桂紅%王廣軍%龔晏青%孫永彊
양계홍%왕엄군%공안청%손영강
爆炸力学%预制破片%飞行规律%梳状靶
爆炸力學%預製破片%飛行規律%梳狀靶
폭작역학%예제파편%비행규률%소상파
explosive mechanics%precast fragments%flying laws%comb targets
为了测量全预制破片在爆轰驱动下的长距离飞行速度,采用梳状靶测量实验方法测量了全预制钨合金破片的飞行速度。介绍了梳状靶测量实验方法原理,给出了典型的梳状靶信号。梳状靶测量实验方法测量的全预制钨合金破片的飞行速度与光幕靶实验方法和理论分析的破片飞行规律进行比较,结果表明,梳状靶实验方法可行,并与高精度的光幕靶测量结果一致。
為瞭測量全預製破片在爆轟驅動下的長距離飛行速度,採用梳狀靶測量實驗方法測量瞭全預製鎢閤金破片的飛行速度。介紹瞭梳狀靶測量實驗方法原理,給齣瞭典型的梳狀靶信號。梳狀靶測量實驗方法測量的全預製鎢閤金破片的飛行速度與光幕靶實驗方法和理論分析的破片飛行規律進行比較,結果錶明,梳狀靶實驗方法可行,併與高精度的光幕靶測量結果一緻。
위료측량전예제파편재폭굉구동하적장거리비행속도,채용소상파측량실험방법측량료전예제오합금파편적비행속도。개소료소상파측량실험방법원리,급출료전형적소상파신호。소상파측량실험방법측량적전예제오합금파편적비행속도여광막파실험방법화이론분석적파편비행규률진행비교,결과표명,소상파실험방법가행,병여고정도적광막파측량결과일치。
In order to measure flying velocities of controlled tungsten alloy fragments under detonation driven, comb targets method was used to study the initial velocities.Schematic of comb targets and typical signal of comb targets were discussed.The experimental results of flying law and long distance flying time of tungsten alloy fragments were validated by laser measurement method and theoretical flying law of fragments.The results show that the comb targets method is feasible.