复杂外形导弹出水过程空化流数值计算研究

基于Zwart-Gerber-Belamri空化模型,采用动网格和复合网格技术,提出了一种复杂外形潜射导弹出水过程中空化流数值计算方法。对头肩部、舵面及突起物的空化生成、演化及影响因素进行了分析。结果表明,出水过程初期空化数降低使附体空泡迅速扩大,随后空泡脱落与振荡的影响将更为显著；肩部在15m/s出水时产生空化并随速度上升而迅速增长, - 攻角时肩空化非对称性显现；舵面空化受出水速度影响较小, 攻角以下时空化面积小于全舵面积的10%,但攻角超过 后空化面积迅速增长至50%以上；减小突起物尺寸有利于避免空化产生,突起物空化受攻角影响较小,但在高速下可诱导临近弹体产生空化。     

AUSMPW+格式在高超声速热化学非平衡流数值模拟中的应用

将AUSMPW+格式应用到高超声速热化学非平衡流场的数值模拟中。为提高精度,采用了三阶MUSCL插值方法。与LU SGS方法结合,提高了单步计算效率和收敛性。采用热化学非平衡十一组元气体模型求解了非定常轴对称Navier Stokes方程组,得到了收敛结果。数值模拟结果与文献结果进行了对比,并在弹道靶中进行了钢质圆球的实验验证。计算结果与文献、实验的对比说明,AUSMPW+格式可以在热化学非平衡流的数值模拟中精确地捕捉到强弓形激波,得到准确的空气动力系数。     

Dynamic evacuation routes for personnel on a naval ship

We propose a dynamic escape route system for emergency evacuation of a naval ship. The system employs signals that adapt to the causative contingency and the crew's physical distribution about the ship. A mixed‐integer nonlinear programming model, with underlying network structure, optimizes the evacuation process. The network's nodes represent compartments, closures (e.g., doors and hatches) and intersections, while arcs represent various types of passageways. The objective function integrates two potentially conflicting factors: average evacuation time and the watertight and airtight integrity of the ship after evacuation. A heuristic solves the model approximately using a sequence of mixed‐integer linear approximating problems. Using data for a Spanish frigate, with standard static routes specified by the ship's designers, computational tests show that the dynamic system can reduce average evacuation times, nearly 23%, and can improve a combined measure of ship integrity by up to 50%. In addition, plausible design changes to the frigate yield further, substantial improvements. Published 2008 Wiley Periodicals, Inc. Naval Research Logistics 2008     

考虑摩擦时环状流的空泡份额求解

在熵增模型的基础上,考虑壁面摩擦对空泡份额的影响,推导出了空泡份额应满足的方程,求得其解析解和数值解,并进行了讨论.分析表明,其结果包含了有关文献的结果,具有更大的适用范围.     

系列头型空泡特征及其对细长体阻力特性影响的试验研究

为了了解不同头型的空泡特征及其对轴对称体阻力特性的影响,在高速水洞中试验研究了6种典型头体在不同空泡数下,轴对称体上空泡的几何特征以及相对应的阻力特性,分析了空泡数对轴对称体空泡特征与阻力的影响.     

谐波平衡法数值模拟周期性非定常流动

谐波平衡法是目前非定常流动数值研究中颇受关注的频域计算方法,该方法计算效率高,特别是对于周期性非定常流动问题具有明显的计算优势。采用谐波平衡法数值模拟高超声速导弹标模模型在不同参数下的强迫俯仰振动,重建气动力/力矩系数迟滞曲线,将计算结果与时域方法相比较,详细考察谐波平衡法的计算精度、效率和内存需求,分析不同参数对谐波平衡法计算的影响。计算结果表明,谐波平衡法适用于中小振幅下的非定常流动计算,且计算时间基本不受减缩频率的影响,对于长周期低频问题,较时域方法有明显计算优势。     

Determining optimal sizes of bounded batches with rejection via quadratic min‐cost flow

In this article, we consider a single machine scheduling problem, in which identical jobs are split into batches of bounded sizes. For each batch, it is allowed to produce less jobs than a given upper bound, that is, some jobs in a batch can be rejected, in which case a penalty is paid for each rejected job. The objective function is the sum of several components, including the sum of the completion times, total delivery cost, and total rejection cost. We reduce this problem to a min‐cost flow problem with a convex quadratic function and adapt Tamir's algorithm for its solution. © 2017 Wiley Periodicals, Inc. Naval Research Logistics 64: 217–224, 2017     

低功率霍尔推力器阳极供气环工程设计关键参数仿真

为了提高低功率霍尔推力器放电通道内中性原子分布均匀性,采用有限元方法对阳极供气环关键结构参数进行优化研究。针对双腔式阳极供气环结构,重点分析了缓冲腔容积比以及缓冲腔隔板导流小孔数量等关键参数对阳极供气均匀性的影响。研究结果表明:随着缓冲腔容积比的增大,阳极供气环出气孔差异率先快速减小后趋于稳定,其中当容积率k=1.0时,平均差异率和最大差异率分别为1.77%和3.79%;隔板间导流小孔数量从8增加到14时,出气孔差异率呈现浴盆曲线特性,其中导流孔数量为10时,平均差异率和最大差异率分别为1.8%和3.8%。研究结果可为霍尔推力器阳极供气环工程设计提供理论支撑。     

预燃室内气氢气氧射流燃烧过程数值分析

建立了液体火箭发动机预燃室内气氢气氧射流燃烧过程的数学模型,包括燃烧过程控制守恒方程、湍流流动方程和湍流燃烧模型,以及求解控制方程所需的辅助关系式;给出了模拟射流燃烧过程的数值方法。对于给定的预燃室结构型式和尺寸,研究了喷嘴构型和氧的喷射方式对化学反应流场和燃烧性能的影响规律。结果表明,喷嘴构型和氧的喷射方式对流动过程和燃烧性能都有影响,且喷嘴结构的影响较为明显。