波浪对水翼非稳态空泡流动特性的影响研究

基于雷诺平均Navier-Stokes方程、Singhal-Et-Al全空化模型和修正的RNG k-ε湍流模型的VOF多相流动数学模型,采用PISO算法的有限体积法和数值水池技术,对波浪作用下NACA0012水翼的非稳态空泡流动特性进行了数值研究,分析了波高和水翼浸深对水翼非稳态空泡的形态演化和脱落频率的影响.计算结果表明:空泡非稳态周期性脱落频率随波高的增加而增加,随水翼浸深的增加而逐渐减小.与无波情况相比,空泡在波谷处提前断裂,空泡形态也因为波谷下方速度场的影响而向上鼓起.由于自由液面的界面效应,空泡形态较无界情况偏扁,并且液面对脱落涡系有吸引作用.     

水下超声速燃气射流动力学特性研究

该文研究水下超声速喷管燃气射流动力学特性.采用基于均质平衡流的mixture多相流模型和标准湍流模式,运用有限体积法和SIMPLE算法,求解了不同工况下的二维水下燃气射流的湍流流动.考虑了流体的可压缩性、黏性、重力作用、气水掺混效应和能量交换等复杂因素.通过对不同扩张比、不同水深和不同来流情况下喷管射流流场的数值计算结果的比较与分析,发现在环境背压较大的情况下,大扩张比喷管燃气射流会产生颈缩、断裂和回击现象;而小扩张比喷管和有来流情况下,喷管燃气射流形态较稳定.     

导弹垂直发射出筒过程中通气空泡流研究

将通气空泡技术应用于导弹水下垂直发射出筒过程,通气空泡是高速航行体获得稳定空泡的一种重要技术。采用基于Mixture多相流模型的有限体积法求解RANS方程,结合动网格技术,对水下垂直发射导弹出筒过程的轴对称流场进行了数值模拟,研究导弹的流体动力特性和通气空泡的演化。结果表明通气空泡可减小导弹出筒过程中的阻力和改善导弹的流体动力载荷。     

潜射导弹水下垂直自抛发射过程研究

研究了潜射导弹水下垂直自抛发射过程中的复杂多相流动问题。采用多相流mixture模型，考虑了流体的可压缩性、黏性、重力作用、气水掺混效应和能量交换等各项因素。应有限体积法（FVM）和Simple算法，求解气水两相混合介质的RANS方程和standard k-ε湍流模式。运用自编UDF模块和动网格技术，实现了导弹出筒过程中弹体运动与气水流场的耦合求解。计算结果揭示了潜射导弹水下垂直自抛发射过程中发动机喷管和发射管内复杂多相流动的演化、流场结构和流体动力特性。     

A numerical analysis of the influence of the cavitator’s deflection angle on flow features for a free moving supercavitated vehicle

When a high-speed cavitated weapon moves under water, the flow properties are important issues for the sake of the trajectory predication and control. In this paper, a single-fluid multiphase flow method coupled with a natural cavitation model is proposed to numerically simulate the flee moving phase of an underwater supercavitated vehicle under the action of the external thrust. The influence of the cavitator＇s deflection angle ranging from -3~ to 3~ on the cavity pattern, the hydrodynamics and the underwater trajectory is investigated. Based on computational results, several conclusions are qualitatively drawn by an analysis. The deflection angle has very little effect on the cavity pattern. When the deflection angle increases, the variation curves of the vertical linear velocity, the lift coefficient and the pitching moment coefficient become flatter. In the phase of the second natural cavitation, at a same time, the greater the deflection angle is, the lower the drag and the lift coefficients will be and the higher the pitching moment coefficient becomes. At the finishing time of the free moving phase, when the deflection angle lies in the small range of -1~ - 1~, the position of the center of mass and the pitching angle of the vehicle are more close to each other. However, when the deflection angle is less than -1° or greater than 1°, the position of the center of mass and the pitching angle change greatly. Ifa proper deflection angle of the cavitator is adopted, the underwater vehicle can navigate in a pseudo-fixed depth.