用合成孔径雷达图像反演浅海水下地形的一种方法

海流与海底地形的相互作用导致了海表面的粗糙起伏,从而引起对海面观测的雷达散射截面的变化。在浅海海流速度垂直分布廓线为均匀的假定下,由流体连续性方程和驰豫时间近似下流体力学弱相互作用的理论,已证明雷达散射截面的空间变化正比于海流方向上海流速度变化的梯度。研究了合成孔径雷达(SAR)对海面的观测图像在无槽道信息和海流方向预知条件下,提出用散射系数的二维相关函数确定海流方向。在海流速度和方向已知条件下,推导了由雷达散射截面的空间变化迭推反演浅海水下地形的公式,并研究了航天飞机SIR-CSAR在我香港特区海域的二维图像反演浅海水下地形的应用。     

新疆博格达南缘后碰撞期陆内裂谷和水下滑塌构造

本文较为系统地研究了哈密市七角井-车轱辘泉和乌鲁木齐市白杨沟地区晚古生代后碰撞期陆内裂谷和滑塌构造的几何学、岩石学和地球化学特征。研究表明,在博格达山南缘的七角井-车轱辘泉一带,玄武岩和流纹岩彼此互层产出,构成厚度较大的后碰撞期双峰式火山岩系,呈近东西方向平行造山带展布,堆积在早二叠世红色磨拉石之上;在白杨沟一带,后碰撞水下滑塌堆积岩与火山岩共存,构成一个厚1300m的滑塌构造剖面,由水下滑塌堆积岩夹双峰式火山岩带、枕状熔岩-气孔状玄武岩带和硅质、泥砂质岩带所组成。其底部以北东走向的拆离断层和晚石炭世灰岩、砂岩岩层接触。在岩石地球化学特征上,火山岩的SiO2含量在53%-67%之间出现间断,呈现双峰式火山岩的特点。其中,流纹岩SiO2平均71.65%,CaO2.15%,Na2O与K2O含量相近(3.2%-3.7%),含碱量>含钙量,ANKC值>1.1;轻稀土富集、稀土总量高,铕亏损,具明显Eu负异常。与之共生的玄武岩则以富硅贫碱为特征,SiO2平均51.05%,TiO2含量变化较大,轻稀土轻度富集,铕异常不明显,属拉斑系列玄武岩类。其特征和东非阿法尔裂谷的双峰式火山岩相近,反映陆内裂谷环境。对滑塌堆积岩带中的辉绿玢岩作锆石U-Pb测年,获289±5Ma年龄值,相当于二叠纪初期。从晚二迭叠世开始,全区处于相对稳定的剥蚀-堆积环境中,形成了厚度较大的磨拉石,并逐渐演化为三叠纪的准平原化环境。     

基于新型分层邻域阈值搜索法提高水下潜器重力匹配导航的匹配效率

本文开展了水下潜器重力匹配导航的匹配效率改善研究.第一,为克服传统TERCOM算法逐点遍历搜索效率较低的缺点,提出新型分层邻域阈值搜索法.其原理如下:首先,利用4格网间隔数进行粗搜索匹配;其次,为提高初始匹配点的选取标准设置4mGal阈值(基准图上重力值与实测重力值之差),对选取的若干粗搜索行最佳匹配点周围24邻域点进行取舍并匹配比较;最后,获得搜索范围内最佳匹配点.第二,综合考虑了重力场标准差、峰度系数、坡度标准差、粗糙度、信息熵等重力场主要特征参数,将其作为适配区优劣的分析依据.第三,在适配性良好的区域内,在保证水下导航精度的前提下,基于分层邻域阈值搜索法,以本文参数设置为例,水下潜器重力匹配导航的匹配效率提高约14.14倍.     

On the determination of the mesh size for numerical simulations of shock wave propagation in near field underwater explosion

It is well known that the accuracy of mesh-based numerical simulations of underwater explosion strongly relies on the mesh size adopted in the analyses. Although a numerical analysis of underwater explosion can be performed with enough accuracy by using considerably fine meshes, such fine meshes may lead to substantially increase in the CPU time and the usage of computer memory. Thus, how to determine a suitable mesh size in numerical simulations is always a problem confronted when attempting to study the shock wave propagation resulting from underwater explosion and the subsequent response of structures. Considering that there is currently no universally accepted method for resolving this problem, this paper aims to propose a simple method to determine the mesh size for numerical simulations of near field underwater explosion. To this end, the mesh size effects on the shock wave propagation of underwater explosion are carefully investigated for different charge weights, through which the correlation between mesh sizes and charge weights is identified. Based on the numerical study, a dimensionless variable (λ), defined as the ratio of the radius of charge to the side length of element, is introduced to be the criterion for determining the mesh size in simulations. It is interesting to note that the presented method is suitable for various charge weights. By using the proposed meshing rule, adequate balance between solution accuracy and computational efficiency can be achieved for different blast scenarios in numerical simulations of underwater explosion.     

Study of a jet-propulsion method for an underwater vehicle

This paper investigates a novel jet-propulsion method for a submerged vehicle. The approach is based on flexible-tube, eccentric rotor, Downingtown-Huber type pumps. Equations of motion are derived for a craft driven by such pumps. In order to develop general insight into the overall dynamics of the system, simulations are carried out for the simple case of horizontal straight-line motion. Results are obtained for the vehicle velocity, distance traveled, pump speed, and energy consumption. Effect of drag forces on the operation of the craft is studied. Finally, the jet-propulsion system is compared with conventional screw-type propulsors via simulation.     

A study of transient responses of a submerged spherical shell under shock waves

Based on a procedure which couples the finite element method with the doubly asymptotic approximation, this work addresses the problem of the transient responses of a submerged spherical shell subjected to strong, plane, incident shock waves, in which elastoplastic material behavior is considered. Simulation results indicate that the procedure adopted shows good agreement with related literature, which considered linear elastic behavior of the shell. Also presented herein are the time histories of surface pressure, radial velocity and von Mises stress of the shell. Moreover, deformation diagrams and spreading of the plastic zone of the shell are described as well.     

海洋声学测温及声层析法

海洋声层析法作为检测海洋内部变化一有力手段，正面临着海洋声学大尺度观测新挑战。本文就海洋声传播的绝热近似；声传播时间的非线性偏移；声速剖面的线性及非线性反演等与声学大尺度观测相关的一些水声学问题的发展现状及存在问题等进行了综述性论述。文中还介绍了赫德岛预演实验等利用声层析法观测海洋内部变化的一些具体应用例     

Transient dynamic response of submerged sphere shell with an opening subjected to underwater explosion

This investigation applies the time domain FEM/DAA coupling procedure to predict the transient dynamic response of submerged sphere shell with an opening subjected to underwater explosions. The elastic–plastic material behavior of the transient fluid–structure interaction relate to structural response equation also presented herein. This analysis also examines the transient responses of structures to different charge distances. The effects of standoff distance on pressure time history of the shell to underwater explosion (3001b TNT) are presented. Additionally, the transient dynamic responses to underwater explosion shockwaves in the sea and the air are compared.     

差分GPS水下地形测绘关键技术研究

简要介绍了将差分GPS技术用于水下地形测绘的方法，重点研究了平面坐标转换和水深数据修正两个关键技术，给出了平面定位的坐标转换方法和考虑水温、含盐度等对声速的影响，以及海水潮位变化等因素后的水深测量修正方法。     

Aspects of the measurement of the acoustic transfer function in a cavitation tunnel

Model scale experiments represent one of the most effective, and probably the most commonly used, approaches for the study of cavitating propeller noise. Despite this, the acquirement of consistent data of propeller noise from tests in model scale facilities is still a challenging task. Data collected with such an approach are usually affected by several scale effects and facility related issues which make such experiments still very complex. Among others, the effect of the facility itself as acoustical surrounding must be carefully addressed in order to properly estimate propeller source levels in ideal free field conditions. This is currently carried out, when possible, by measuring facility transfer functions and applying such functions as a correction to measured noise spectra. The development of robust procedures for the measurement of these transfer functions is thus very important. In the present work, this problem is addressed by discussing in details techniques, merits and possible problems related to this topic.