波浪对有梁面板结构冲击作用数值模拟

采用计算机数值模拟方法,在FLUENT软件计算平台上建立了二维规则波数值波浪水槽,对透空有梁面板结构底面受到的波浪冲击作用进行研究。数学模型采用RANS方程和k-ε湍流模型,以VOF方法处理自由表面。通过对不同工况的数值模拟和试验结果比较,验证了模型的造消波性能和应用的有效性。通过计算,得到了波浪冲击过程中波陡、超高和板宽各因素对冲击压强的影响。最后在已有冲击压强计算公式基础上提出了修正公式,以更准确地预报波浪的冲击荷载,深入认识波浪冲击机理。     

港珠澳大桥长寿命海工高性能混凝土配制

针对120 a设计使用年限要求,阐述港珠澳大桥不同主体结构海工高性能混凝土基本性能设计的原则。在暴露试验得出的混凝土长期耐久性影响因素的基础上,系统研究配合比参数对混凝土性能的影响,介绍满足桥梁、隧道等不同结构工作性、强度、耐久性及体积稳定性要求的长寿命海工高性能混凝土的配制基本思路与方法。     

码头面高程计算方法探讨

针对码头项面高程确定中遇到的实际问题,提出一种新的计算方法。新方法在吸收现行规范中有掩护式码头和开敞式码头顶面高程计算方法特点的基础上,对于各种掩护程度码头采用统一公式,可以避开因半开敞式码头界定的不明确性给码头顶面高程计算带来的麻烦,在考虑波浪荷载与水位组合方面概念更清晰,应用较方便。     

三维水弹性软件并行化的初步实现

为了满足超大型浮体尺寸巨大、结构复杂的分析需求,以及三维水弹性软件商用化的快速计算要求,文章通过对已有三维水弹性程序的分析,设计并实现了多参数并行化快速计算,为超大型浮体进一步水弹性分析奠定了良好基础。文中以常规船舶和超大型浮式平台为例,测试了并行化软件的正确性与快速性。结果表明,并行化改造达到了快速计算的效果。     

动态对动态差分相对定位方法建模与测试

揭示了传统的GNSS差分处理技术在基准站移动时所面临的问题,从差分实现的原理上首次对该问题进行了理论解释。针对这一问题建立了动态对动态差分相对定位模型,提出了测试方案并进行相应的试验验证,结果表明:所提动态对动态差分相对定位方法精度达到10cm量级,能够满足高精度动态对动态测量需求。     

低阻通风船体的远程控制测试平台开发（英文）

This paper addresses the development and testing of a remotely controlled boat platform with an innovative air-ventilated hull. The application of air cavities on the underside of ship hulls is a promising means for reducing hydrodynamic drag and pollutant emissions and increasing marine transportation efficiency. Despite this concept’s potential, design optimization and high-performance operation of novel air-cavity ships remain a challenging problem. Hull construction and sensor instrumentation of the model-scale air-cavity boat is described in the paper. The modular structure of the hull allows for easy modifications, and an electric propulsion unit enables self-propelled operation. The boat is controlled remotely via a radio transmission system. Results of initial tests are reported, including thrust, speed, and airflow rate in several loading conditions. The constructed platform can be used for optimizing air-cavity systems and testing other innovative hull designs. This system can be also developed into a high-performance unmanned boat.     

A havelock source panel method for near-surface submarines

A panel method is described for calculating potential flow around near-surface submarines. The method uses Havelock sources which automatically satisfy the linearized free-surface boundary condition. Outputs from the method include pressure field, pressure drag, wave resistance, vertical force, trim moment and wave pattern. Comparisons are made with model tests for wave resistance of Series 58 and DARPA SUBOFF hulls, as well as with wave resistance, lift force and trim moment of three length-to-diameter variants of the DSTO Joubert submarine hull. It is found that the Havelock source panel method is capable of determining with reasonable accuracy wave resistance, vertical force and trim moment for submarine hulls. Further experimental data are required in order to assess the accuracy of the method for pressure field and wave pattern prediction. The method is implemented in the computer code “HullWave” and offers potential advantages over RANS-CFD codes in terms of speed, simplicity and robustness.     

A non-geometrically similar model for predicting the wake field of full-scale ships

The scale effect leads to large discrepancies between the wake fields of model-scale and actual ships, and causes differences in cavitation performance and exciting forces tests in predicting the performance of actual ships. Therefore, when test data from ship models are directly applied to predict the performance of actual ships, test results must be subjected to empirical corrections. This study proposes a method for the reverse design of the hull model. Compared to a geometrically similar hull model, the wake field generated by the modified model is closer to that of an actual ship. A non- geometrically similar model of a Korean Research Institute of Ship and Ocean Engineering (KRISO)’s container ship (KCS) was designed. Numerical simulations were performed using this model, and its results were compared with full-scale calculation results. The deformation method of getting the wake field of full-scale ships by the non-geometrically similar model is applied to the KCS successfully.     

Experimental and numerical investigations on vibration characteristics of a loaded ship model

In this paper, vibration characteristics of the structure in the finite fluid domain are analyzed using a coupled finite element method. The added mass matrix is calculated with finite element method (FEM) by 8-node acoustic fluid elements. Vibration characteristics of the structure in finite fluid domain are calculated combining structure FEM mass matrix. By writing the relevant programs, numerical analysis on vibration characteristics of a submerged cantilever rectangular plate in finite fluid domain and loaded ship model is performed. A modal identification experiment for the loaded ship model in air and in water is conducted and the experiment results verify the reliability of the numerical analysis. The numerical method can be used for further research on vibration characteristics and acoustic radiation problems of the structure in the finite fluid domain.     

Numerical calculation of supercavitating flows over the disk cavitator of a subsonic underwater projectile

To deal with the effect of compressible fluids on the supercavitating flow over the subsonic disk cavitator of a projectile, a finite volume method is formulated based on the ideal compressible potential theory. By using the continuity equation and Tait state equation as well as Riabouchinsky closure model, an “inverse problem” solution is presented for the supercavitating flow. According to the impenetrable condition on the surface of supercavity, a new iterative method for the supercavity shape is designed to deal with the effect of compressibility on the supercavity shape, pressure drag coefficient and density field. By this method, the very low cavitation number can be computed. The calculated results agree well with the experimental data and empirical formula. At the subsonic condition, the fluid compressibility will make supercavity length and radius increase. The supercavity expands, but remains spheroid. The effect on the first 1/3 part of supercavity is not obvious. The drag coefficient of projectile increases as the cavitation number or Mach number increases. With Mach number increasing, the compressibility is more and more significant. The compressibility must be considered as far as the accurate calculation of supercavitating flow is concerned.