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
5期
14-18
,共5页
水下航行体%多相流%排气%气泡
水下航行體%多相流%排氣%氣泡
수하항행체%다상류%배기%기포
Underwater vehicle%Multiphase flow%Exhaust%Bubble
针对航行体排气水下发射流体动力问题,采用VOF(Volume of Fluid)多相流模型、标准湍流模型,结合动网格技术,进行发射过程流场数值仿真,获得了航行体表面压力分布及气泡的发展过程,计算结果与试验结果吻合较好;利用形成的数值方法,研究了发射深度、出筒速度对排气气泡发展过程的影响,获得了对工程设计具有参考价值的结论。
針對航行體排氣水下髮射流體動力問題,採用VOF(Volume of Fluid)多相流模型、標準湍流模型,結閤動網格技術,進行髮射過程流場數值倣真,穫得瞭航行體錶麵壓力分佈及氣泡的髮展過程,計算結果與試驗結果吻閤較好;利用形成的數值方法,研究瞭髮射深度、齣筒速度對排氣氣泡髮展過程的影響,穫得瞭對工程設計具有參攷價值的結論。
침대항행체배기수하발사류체동력문제,채용VOF(Volume of Fluid)다상류모형、표준단류모형,결합동망격기술,진행발사과정류장수치방진,획득료항행체표면압력분포급기포적발전과정,계산결과여시험결과문합교호;이용형성적수치방법,연구료발사심도、출통속도대배기기포발전과정적영향,획득료대공정설계구유삼고개치적결론。
Aiming at issues concerning the flow dynamics of underwater vehicle launching with exhaust, the numerical simulation on the flow field of underwater launching process was established. Combining VOF multiphase flow model, the standard turbulence model,and the technique of dynamic mesh, characteristics of the distribution of pressure on the vehicle's surface and the forming process of exhausting bubble were obtained and the numerical result agreed well with those in experiments. The influence of depth of launch and velocity outside tube on the forming process of bubble is numerically studied and some conclusions are achieved which have important reference value to engineering application.