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分层海洋中运动物体生成的内波 被引量:5
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作者 徐肇廷 姚凤朝 隋红波 《青岛海洋大学学报(自然科学版)》 CSCD 北大核心 2001年第4期461-466,共6页
该文提供分层海洋中运动物体生成内波的理论、数值和实验研究的背景资料的综述 ,并给出理论研究的 Green函数、正交模态模式和极点回避等方法的评述。数值研究给出数值求解Wronsky行列式的源求解方法及介绍直接差分计算含源内波方程和... 该文提供分层海洋中运动物体生成内波的理论、数值和实验研究的背景资料的综述 ,并给出理论研究的 Green函数、正交模态模式和极点回避等方法的评述。数值研究给出数值求解Wronsky行列式的源求解方法及介绍直接差分计算含源内波方程和积分方程的方法。有关源致内波的实验研究 ,作者介绍物体在分层流水槽运动时生成内波的两个典型实验及其主要实验结果。最后评述船舶在海洋表面处生成表面波的研究方法 ,以此指导水下 Rankine卵形体生成内波的实验研究。 展开更多
关键词 分层海洋 内波 波阻 生成机制 诱导阻 升力实验
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扑旋翼刚度和翼梢形状对气动升力和效率的影响 被引量:2
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作者 贺媛媛 张航 +1 位作者 王琦琛 杨炫 《航空学报》 EI CAS CSCD 北大核心 2023年第12期139-156,共18页
具有垂直起降及悬停性能的扑旋翼刚度分布和形状对其气动升力和效率的影响与传统仿昆虫扑翼明显不同。针对扑旋翼刚度和翼梢形状对其悬停飞行模式下的气动升力和效率的影响开展实验研究,研制了12种不同结构构型及翼梢后掠角的传统矩形... 具有垂直起降及悬停性能的扑旋翼刚度分布和形状对其气动升力和效率的影响与传统仿昆虫扑翼明显不同。针对扑旋翼刚度和翼梢形状对其悬停飞行模式下的气动升力和效率的影响开展实验研究,研制了12种不同结构构型及翼梢后掠角的传统矩形扑旋翼样件和一种仿蜻蜓翅外形的扑旋翼样件,通过实验测试定量分析了各扑旋翼样件的展向和弦向刚度、翼梢刚度及形状对其运动、气动升力和效率的影响。结果表明,弦向刚度和翼梢形状对扑旋翼运动影响显著,优化展向和弦向刚度分布对翼膜的支撑和采用仿蜻蜓翅梢形状可显著提高扑旋翼的气动升力和效率。以本实验中采用的重量为30.1 g的扑旋翼模型为例,在输入电压3.4 V时,优化后的仿生扑旋翼平均升力(49.6 g)比初始矩形扑旋翼提高74%,升力效率从3.5 g/W提高到5.9 g/W。本研究对扑旋翼微型飞行器气动性能的提升具有重要意义。 展开更多
关键词 扑旋翼微型飞行器 仿生扑旋翼 扑旋翼刚度 翼梢形状 气动 升力实验
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Experimental investigation of particle-induced pressure loss in solid–liquid lifting pipe 被引量:6
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作者 宋跃文 朱小军 +1 位作者 孙志强 唐达生 《Journal of Central South University》 SCIE EI CAS CSCD 2017年第9期2114-2120,共7页
In order to investigate the characteristics of particle-induced pressure loss in the solid–liquid lifting pipe,a series of experiments were conducted in 200 mm diameter lifting pipe.Simulation manganese nodules with ... In order to investigate the characteristics of particle-induced pressure loss in the solid–liquid lifting pipe,a series of experiments were conducted in 200 mm diameter lifting pipe.Simulation manganese nodules with five different mean diameters of10 mm,20 mm,30 mm,40 mm and 50 mm were used,both in isolation and a combination in equal fraction by mass.The flow velocities in the lifting pipe ranged from 0.12 m/s to 1.61 m/s,and the mass of particles employed was 10 kg for each particle diameter.Three regimes,wavy bed,partly fluidization,and fully fluidization,were observed over the flow velocity.The solid–liquid pressure drop data were measured by differential pressure transmitter,and pressure drop caused by the solid particles was calculated and analyzed.The results show that the evolutions of the pressure loss due to solid particles are relevant to the solid–liquid flow regimes,and they are distinctly influenced by fluid velocity and particle size. 展开更多
关键词 lifting pipe pressure loss simulation manganese nodules flow regimes
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Experimental study on heat transfer of aviation kerosene in a vertical upward tube at supercritical pressures 被引量:8
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作者 黄丹 阮波 +6 位作者 吴晓雨 张巍 徐国强 陶智 姜培学 马连湘 李蔚 《Chinese Journal of Chemical Engineering》 SCIE EI CAS CSCD 2015年第2期425-434,共10页
A research on the heat transfer performance of kerosene flowing in a vertical upward tube at supercritical pressure is presented.In the experiments,insights are offered on the effects of the factors such as mass flux,... A research on the heat transfer performance of kerosene flowing in a vertical upward tube at supercritical pressure is presented.In the experiments,insights are offered on the effects of the factors such as mass flux,heat flux,and pressure.It is found that increasing mass flux reduces the wall temperature and separates the experimental section into three different parts,while increasing working pressure deteriorates heat transfer.The extended corresponding-state principle can be used for evaluating density and transport properties of kerosene,including its viscosity and thermal conductivity,at different temperatures and pressures under supercritical conditions.For getting the heat capacity,a Soave–Redlich–Kwong(SRK)equation of state is used.The correlation for predicting heat transfer of kerosene at supercritical pressure is established and shows good agreement with the experimental data. 展开更多
关键词 Supercritical pressure KEROSENE Heat transfer
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