On the axial force induced on a duct by a propulsor

The axial force induced on a duct (duct thrust) which surrounds a propulsor is, by means of an energy conservation argument, expressed in terms of the thrust and power of the propulsor and the kinetic energy losses per unit of time of the propulsor and the duct. Emphasis is put on the linear theory of an axisymmetric ducted actuator disk, where it is shown that the work done by the duct thrust is equal to the extra work done by the actuator disk when it is surrounded by the duct. This simplified model gives more insight into the interaction between the propeller and the duct and on the limits of linearization.     

导管式推进器非定常性能数值计算方法研究

基于滑移网格方法，采用SST k-ω湍流模型研究不同网格划分方式对带前置定子导管式推进器非定常性能的研究。首先基于相对参考坐标系法及滑移网格方法分别对推进器在定常与非定常下的性能进行数值预报，并与试验结果相比验证计算方法的可靠性。基于该方法研究整体网格划分方式与周期性网格对推力系数、扭矩系数与推进器各个方向上的非定常脉动力的影响。研究结果为进一步研究推进器非定常性能提供了参考。     

图像处理技术在船舶推进器空泡试验中的应用研究

运用数字图像技术和AutoCAD2000图形软件，探索了处理螺旋桨桨叶上空泡图像的问题，利用桨叶空间曲面网格和桨叶空泡图像对比的方式给出了浆叶上空泡区域的边缘，同时还指出了使这一技术实用化需要作的工作。对于空泡体积这一问题，提出了结构光方式的测量模型，它比已报道的同类方法有较高的操作效率。     

Experimental study on a model azimuthing podded propulsor in ice

The objective of this study was to investigate the performance of a model azimuthing podded propulsor in ice-covered water. Model tests were carried out with two different depths of cut into the ice (15 and 35 mm), two different ice conditions (presawn and pack ice conditions), and four different azimuthing angles. The depth of cut is the maximum penetration depth of the propeller blade into the ice block. The 0.3-m-diameter model propeller was operated in a continuous ice milling condition. Ice loads were measured by several sensors which were installed in various positions on the model. Six one-axis pancake-style load cells on the top of the model measured the global loads and two six-component dynamometers were installed on the shaft to measure the shaft loads. One six-component dynamometer was attached to the one of the propeller blades inside the hub to measure the blade loads. The pod unit and propeller performance in ice are presented. Ice-related loads, which were obtained when the blade was inside the ice block, are introduced and discussed. During the propeller–ice interaction, a blade can experience the path generated by the previous blade, which is called the shadowing effect. The effects of shadowing, depth of cut, azimuthing angle, and advance coefficient on propulsor performance are presented and discussed.     

几何参数对组合式推进器流噪声水平的影响

在组合式推进器相同水动力性能的设计前提下,采用数值模拟的方法针对不同设计方案流噪声水平进行了计算。宽带噪声采用Proudman声功率模型及Lilley提出的AALS模型计算,线谱噪声采用径向脉动力幅值衡量,比较了不同方案不同几何参数下的噪声,并在此基础上总结出主要几何参数与噪声水平之间的关系。本文研究成果对进一步进行组合式推进器声学设计具有重要指导意义。     

L形吊舱推进器水动力性能CFD研究

应用CFD方法,对某L形吊舱推进器在敞水中的直航(长航)及斜航(机动)水动力性能进行数值模拟与分析研究.分别采用多参考系准定常模型、混合面定常模型及滑移网格非定常模型进行了计算,比较了不同计算模型对推进器水动力预报结果的影响,并分析了水动力(矩)及流场随舵角的变化规律.     

影响某艇喷水推进器推进性能的若干因素

基于某艇的推进性能需求,以喷水推进器设计工况为分析对象,采用计算流体力学（Computational Fluid Dynamics,CFD）方法,建立计算模型,研究叶轮叶顶间隙、流道格栅密度、艇底水底间距、双泵轴间距等工程应用因素对推进性能的影响,可为某艇喷水推进器的设计、安装与使用等提供合理依据。     

吊舱式电力推进系统的特点与应用

对目前流行的吊舱式船舶电力推进系统的特点进行了简要的分析和对比,指出船舶电力推进广泛应用已是一个必然的趋势;随后,对船舶电力推进系统应用的几个问题谈了几点思考。     

船体与组合推进器系统推力减额特性设计主参数和优化策略研究

在文献[1]的基础上,提出了评价船后组合推进器推力减额特性的4个指标:整体推力减额效率(1-t1)、转子推力减额效率(1-t2)、组合推进器推力比τ和导管定子阻力比γ.利用CSSRC现存试验数据运用简单对比和统计分析方法,给出了诸设计参数对这些指标影响的显著性和规律性.推荐采用受控于全部主参数的指标(1-t2)作为船体与组合推进器相互干扰特性优化的总目标,提出了用部分主参数控制的对应分目标优化和迭代来实现总目标优化的简明策略.实例计算表明,优化设计船体尾型主参数LRD、CPR和推进器主参数(A)ex/AP的搭配,可大幅度提高船后组合推进器的推力减额效率.     

导管螺旋桨内流场的LDV测量

为了探讨导管内流场,通过在导管壁上开窗口,使用LDV激光穿过窗口方案来测量导管螺旋桨的内流场.测量结果表明该方案测量导管内流场是可行的,并为导管内螺旋桨叶片的环量分布分析提供了条件.