船舶力学
船舶力學
선박역학
JOURNAL OF SHIP MECHANICS
2011年
9期
960-968
,共9页
何春涛%王聪%魏英杰%王柏秋
何春濤%王聰%魏英傑%王柏鞦
하춘도%왕총%위영걸%왕백추
垂直入水空泡%空泡内压强%VOF%自由水面
垂直入水空泡%空泡內壓彊%VOF%自由水麵
수직입수공포%공포내압강%VOF%자유수면
vertical water-entry cavity%cavity pressure%VOF%free water surface
基于RANS方程,在VOF多相流模型中嵌入水蒸汽和水之间的质量输运模型成功实现了垂直入水空泡流的数值计算.通过与试验结果的对比说明了以上数值方法的可信性,并在此基础之上对带不同锥角头型圆柱体以不同速度垂直撞击自由液面后所生成的空泡内部压强分布进行了深入分析,结果表明:在入水空泡形成阶段,空泡内部压强会出现较大的降低现象,并随着空泡的发展压强值逐渐趋于稳定;空泡形成阶段空泡内部压强随入水物体头部锥角增加而增加;在开空泡阶段空泡内部压强低于环境压强,并随着入水速度增加而呈降低变化趋势,空泡内部压强轴向和径向分布较为稳定,没有较大的压强梯度;在空泡趋于闭合阶段空泡内部压强出现较大的波动,其变化规律与空泡内部空气复杂速度场变化规律相吻合.
基于RANS方程,在VOF多相流模型中嵌入水蒸汽和水之間的質量輸運模型成功實現瞭垂直入水空泡流的數值計算.通過與試驗結果的對比說明瞭以上數值方法的可信性,併在此基礎之上對帶不同錐角頭型圓柱體以不同速度垂直撞擊自由液麵後所生成的空泡內部壓彊分佈進行瞭深入分析,結果錶明:在入水空泡形成階段,空泡內部壓彊會齣現較大的降低現象,併隨著空泡的髮展壓彊值逐漸趨于穩定;空泡形成階段空泡內部壓彊隨入水物體頭部錐角增加而增加;在開空泡階段空泡內部壓彊低于環境壓彊,併隨著入水速度增加而呈降低變化趨勢,空泡內部壓彊軸嚮和徑嚮分佈較為穩定,沒有較大的壓彊梯度;在空泡趨于閉閤階段空泡內部壓彊齣現較大的波動,其變化規律與空泡內部空氣複雜速度場變化規律相吻閤.
기우RANS방정,재VOF다상류모형중감입수증기화수지간적질량수운모형성공실현료수직입수공포류적수치계산.통과여시험결과적대비설명료이상수치방법적가신성,병재차기출지상대대불동추각두형원주체이불동속도수직당격자유액면후소생성적공포내부압강분포진행료심입분석,결과표명:재입수공포형성계단,공포내부압강회출현교대적강저현상,병수착공포적발전압강치축점추우은정;공포형성계단공포내부압강수입수물체두부추각증가이증가;재개공포계단공포내부압강저우배경압강,병수착입수속도증가이정강저변화추세,공포내부압강축향화경향분포교위은정,몰유교대적압강제도;재공포추우폐합계단공포내부압강출현교대적파동,기변화규률여공포내부공기복잡속도장변화규률상문합.
Pressure distribution in vertical water-entry cavity is investigated computationally.Particular attention is given to the simulation method based on solving the time dependent Reynolds-averaged Navier-Stokes equations and the VOF (fractional volume of fluid) multiphase method with cavitation mass transfer model,and turbulence closure.Numerical results compared favorably with the experimental data show that the numerical method in this paper is able to capture the pressure evolution in the vertical water entry cavity properly.Pressure distributions in cavity are discussed for various entry speeds and nose shapes projectiles,numerical results show that the pressure drop in cavity is dependent on the entry velocity in open-cavity period,the pressure drop increases with the increment of entry velocity,In surface closure period,the pressure in the cavity presents complicated fluctuation features and the airflow velocity value increases too many times greater than the entry velocity.