鱼雷技术
魚雷技術
어뢰기술
TORPEDO TECHNOLOGY
2013年
3期
161-164
,共4页
邱海强%袁绪龙%王亚东%刘传龙
邱海彊%袁緒龍%王亞東%劉傳龍
구해강%원서룡%왕아동%류전룡
回转体%入水冲击%空泡形态%混合物模型%冲击载荷
迴轉體%入水遲擊%空泡形態%混閤物模型%遲擊載荷
회전체%입수충격%공포형태%혼합물모형%충격재하
axisymmetric body%water entry impact%cavity shape%MIXTURE model%impact load
回转体入水问题对导弹、鱼雷等的外形和弹道设计有着深远影响。本文利用商业软件 FLUENT 6.3,结合动网格技术和用户自定义函数(UDF),使用混合物(MIXTURE)模型对平头、锥头和圆头回转体在速度为50~150 m/s 时的入水过程进行了仿真试验,探究速度和头型对其入水冲击载荷和空泡形态的影响。试验结果表明,回转体高速入水冲击载荷峰值发生在入水初期,且速度增大时,回转体冲击载荷、空泡直径和长度亦随之增大,在速度相同的情况下,回转体冲击载荷、空泡直径和长度按平头、锥头、圆头的次序依次减小。
迴轉體入水問題對導彈、魚雷等的外形和彈道設計有著深遠影響。本文利用商業軟件 FLUENT 6.3,結閤動網格技術和用戶自定義函數(UDF),使用混閤物(MIXTURE)模型對平頭、錐頭和圓頭迴轉體在速度為50~150 m/s 時的入水過程進行瞭倣真試驗,探究速度和頭型對其入水遲擊載荷和空泡形態的影響。試驗結果錶明,迴轉體高速入水遲擊載荷峰值髮生在入水初期,且速度增大時,迴轉體遲擊載荷、空泡直徑和長度亦隨之增大,在速度相同的情況下,迴轉體遲擊載荷、空泡直徑和長度按平頭、錐頭、圓頭的次序依次減小。
회전체입수문제대도탄、어뢰등적외형화탄도설계유착심원영향。본문이용상업연건 FLUENT 6.3,결합동망격기술화용호자정의함수(UDF),사용혼합물(MIXTURE)모형대평두、추두화원두회전체재속도위50~150 m/s 시적입수과정진행료방진시험,탐구속도화두형대기입수충격재하화공포형태적영향。시험결과표명,회전체고속입수충격재하봉치발생재입수초기,차속도증대시,회전체충격재하、공포직경화장도역수지증대,재속도상동적정황하,회전체충격재하、공포직경화장도안평두、추두、원두적차서의차감소。
The problem of high-speed water entry of an axisymmetric body greatly influences the design of shape and trajectory for a torpedo or a missile. This paper simulates the impact and cavity shape in water entry of different head shapes, such as flat head, cone head, and round head, at the velocity between 50~150 m/s with the commercial software FLUENT6.3 combining with the dynamic mesh, user-define function(UDF) and MIXTURE model. Conclusions are drawn that the peak of impact load appears in the primary period of the water entry; the impact load and the cavity′s length and diameter increase with the increasing velocity; while the impact load and the cavity′s length and diameter decrease in the order of flat head, cone head, and round head when the bodies have same velocity.