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91.
In order to protect the vulnerable turbine components from extreme high temperature, coolant flow is introduced from the compressor to the disk cavity, inevitably interacting with the main flow. This paper describes an experimental investigation of the interaction between the main flow and the purge flow in a low-speed turbine cascade with three purge flow rates, Cm = 0, Cm = 1%, and Cm = 2%. In order to study the effect of the interaction between the main flow and the purge flow on the secondary flows, a Rortex method developed by Liu Chaoquan is introduced to identify the vortex in the flow field. In the meantime, a method to calculate the mean entropy production rate based on the particle image velocimetry (PIV) result is adopted to investigate the flow loss. The PIV result indicates that the purge flow has a prominent impact on the flow field of the cascade passage, changing the velocity distribution that induces a local blockage area. The results of vortex identification show that the purge flow promotes the generation of the passage vortex near the suction side. In addition, the purge flow makes the passage vortex migrate to the tip wall direction, enlarging the region affected by the secondary flow. The mean entropy production (MEP) result shows that the flow loss is mainly caused by the passage vortex. The coincidence of the high-MEP region and the location of the passage vortex indicates that the purge flow increases the secondary flow loss by affecting the formation and the migration of the passage vortex. 相似文献
92.
Propagation dynamics of the cosh-Airy vortex(CAiV) beams in a chiral medium is investigated analytically with Huygens–Fresnel diffraction integral formula. The results show that the CAiV beams are split into the left circularly polarized vortex(LCPV) beams and the right circularly polarized vortex(RCPV) beams with different propagation trajectories in the chiral medium. We mainly investigate the effect of the cosh parameter on the propagation process of the CAiV beams.The propagation characteristics, including intensity distribution, propagation trajectory, peak intensity, main lobe's intensity, Poynting vector, and angular momentum are discussed in detail. We find that the cosh parameter affects the intensity distribution of the CAiV beams but not its propagation trajectory. As the cosh parameter increases, the distribution areas of the LCPV and RCPV beams become wider, and the side lobe's intensity and peak intensity become larger. Besides, the main lobe's intensity of the LCPV and RCPV beams increase with the increase of the cosh parameter at a farther propagation distance, which is confirmed by the variation trend of the Poynting vector. It is significant that we can vary the cosh parameter to control the intensity distribution, main lobe's intensity, and peak intensity of the CAiV beams without changing the propagation trajectory. Our results may provide some support for applications of the CAiV beams in optical micromanipulation. 相似文献
93.
Chao Tian Yuanli Liang Haixia Lin Jie Song Qi Li Rui Li 《Journal of Dispersion Science and Technology》2019,40(6):892-900
A rosin-based ester tertiary amine salt (RETAS) cationic surfactant was obtained using natural rosin as raw material. GC-MS of RETAS was detailed analyzed. The pH-responsive mechanism of rosin-based ester tertiary amine (RETA) and RETAS was confirmed by applying theoretical calculations about electrostatic potential maps of RETA and RETAS cation using Gaussian software. Mixed system surfactants were obtained by blending RETAS cationic surfactant with sodium dodecyl benzene sulfonate (SDBS) anionic surfactant. The binary mixed surfactant systems of RETAS and SDBS had obvious synergistic effect. The γcmc and CMC were 39.40?mN/m and 0.56?mmol/L at the optimum molar fraction of RETAS (α)?=?0.6, respectively. The stability time of emulsion with the optimum mixed system as emulsifier increased to 309?s at α?=?0.6. The emulsifying capacity of RETAS was much better than that of RETA. RETAS had pH-responsive targeted release and the optimum mixed system showed a relatively sustained drug release by using doxorubicin (DOX) as a model drug. These results indicate that RETAS surfactant and mixed system surfactant are both promising for applications in drug delivery and emulsification. 相似文献
94.
制备了多孔碳固载离子液体纳米材料修饰玻碳电极(GCE),用于抗氧化剂叔丁基对苯二酚(TBHQ)的检测研究。不同电极上的交流阻抗结果表明,经过多孔碳固载离子液体修饰后的玻碳电极阻抗显著减小。多孔碳固载离子液体修饰后电极的氧化峰电流为41.93μA,比修饰前增大约5.5倍,说明多孔碳固载离子液体可显著提高电极的导电性,促进电极表面的电子转移,提高检测灵敏度。用时间~电流曲线测得TBHQ的线性范围为1.00~120.00μg/mL,检出限为0.16μg/mL。 相似文献
95.
96.
Sergio Rica 《Comptes Rendus Mecanique》2019,347(4):365-375
As shown by Crow in 1970, the evolution of two almost parallel vortex filaments with opposite circulation exhibits a long-wave instability. Ultimately, the symmetric mode increases its amplitude reconnecting both filaments and ending into the formation of an almost periodic structure of vortex rings. This is a universal process, which appears in a wide range of scales: from the vortex trails behind an airplane to a microscopic scale of superfluids and Bose–Einstein condensates. In this paper, I will focus on the vortex reconnection for the latter case by employing Gross–Pitaevskii theory. Essentially, I focus on the well-known laws of interaction and motion of vortex filaments. By means of numerical simulations, as well as theoretically, I show that a self-similar finite-time dynamics manifests near the reconnection time. A self-similar profile is selected showing excellent agreement with numerical simulations. 相似文献
97.
旋涡与行进表面水波相互作用的实验研究 总被引:1,自引:0,他引:1
采用振动板式造波器在二维水槽中生成近似单色的行进表面水波,采用夹板式涡发生器生成稳定上浮的涡对,在Froude数约为0.5的条件下,得到了水下涡对与不同波长和振幅的行进表面水波相互作用时的干扰图象,以实验方法验证了理论分析和数值计算的结果,并为进一步研究旋涡与行进表面水波的相互作用提供了一种实验研究方法 相似文献
98.
99.
在应力代数模型基础上引入密度状态方程建立了变密度的各向异性湍浮力射流模型,并给出了浮力系数的简单计算式.对存在密度差的射流进行了数值计算,所得轨迹线与实验结果吻合良好.应用有限体积法对流动环境中不同喷角二维立面射流流场特性进行了数值分析,对涡心及分离点位置与喷角关系的结果分析表明喷角为90°时回流区域最大.提出了面积湍动能kA概念,以此分析了流体间的掺混强度与喷角间的关系,结果表明喷角为90°时最有利于射流水体与环境水体间的掺混. 相似文献
100.
通过PISO方法求解非定常不可压N-S方程,研究小展弦比反齐默曼机翼在低雷诺数下的流场特征,并分析其对气动特性的影响.结果显示前缘分离涡在反齐默曼机翼上表面形成一对集中涡.分析表明这对集中涡是影响反齐默曼机翼气动特性的主要因素,给机翼提供了较大的非线性升力和较大的失速攻角,前缘涡之间的相互影响使得机翼出现非定常现象和大攻角的非对称现象.与矩形翼相比,反齐默曼机翼有较好的稳定性. 相似文献