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小流量工况下汽轮机末级的脱流特性研究 被引量:4
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作者 赵金峰 冯忠宝 +2 位作者 曹丽华 司和勇 姚莹莹 《汽轮机技术》 北大核心 2019年第3期192-194,共3页
利用CFX软件对小流量下汽轮机低压缸末级叶片的脱流特性进行研究。结果表明:在额定背压、G1/G0=0.3工况下,动静叶间隙开始形成脱流涡。随着流量的减小,脱流涡沿叶高向叶根方向发展。当G1/G0=0.08时,脱流涡几乎占据整个叶高,涡核由72.7%... 利用CFX软件对小流量下汽轮机低压缸末级叶片的脱流特性进行研究。结果表明:在额定背压、G1/G0=0.3工况下,动静叶间隙开始形成脱流涡。随着流量的减小,脱流涡沿叶高向叶根方向发展。当G1/G0=0.08时,脱流涡几乎占据整个叶高,涡核由72.7%相对叶高迁移到49.1%,严重恶化末级流场,威胁叶片安全。 展开更多
关键词 汽轮机 末级叶片 小流量工况 脱流涡
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Characteristics of a Supersonic Swirling Dehydration System of Natural Gas 被引量:24
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作者 刘恒伟 刘中良 +2 位作者 冯永训 顾克宇 颜廷敏 《Chinese Journal of Chemical Engineering》 SCIE EI CAS CSCD 2005年第1期9-12,共4页
A new type of dehydration unit for natural gas was briefly described and its basic structure and working principles were presented. An indoor test rig for testing the unit performance was set up and the experimental r... A new type of dehydration unit for natural gas was briefly described and its basic structure and working principles were presented. An indoor test rig for testing the unit performance was set up and the experimental results were given. The results showed that the unit could attain a maximum dew point depression of about 20℃ without any need of external mechanical power and chemicals. The pressure loss ratio, shock wave and the flow rate had great influence on the dehydration characteristics. From the systematic analysis of the factors that affect the dehydration efficiency of the unit, the suggestions for improving the unit are put forward. 展开更多
关键词 supersonic swirling separator DEHYDRATION natural gas
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Flow characteristics at low Reynolds number around two in-line circular cylinders with slits 被引量:1
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作者 SUN Zhi-qiang ZHANG Yu-zhuo +1 位作者 XING Peng-fei LI Sai-wei 《Journal of Central South University》 SCIE EI CAS CSCD 2019年第8期2021-2028,共8页
This study investigated numerically the characteristics of laminar flow around two identical circular cylinders placed in tandem, with slits of the same width through their respective axis. The center to center distan... This study investigated numerically the characteristics of laminar flow around two identical circular cylinders placed in tandem, with slits of the same width through their respective axis. The center to center distance between the cylinders and the slit orientation were varied to study their effects on the flow structure, lift and drag, and vortex shedding characteristics. It was found that three flow regimes could be distinguished, the transitions between which could be indicated by the sudden changes in drag and lift. Asymmetrically, configured slits destabilized the stagnant region between cylinders;whereas in-line slits connect the two cylinders to act as a single elongated bluff body, even at large cylinder separation, by stabilizing the stagnant region in between. These in turn strongly modified the transition between flow regimes. Vortex shedding was also strongly influenced by both slit configuration and cylinder separation. 展开更多
关键词 two cylinders in tandem circular cylinder with slit vortex shedding laminar wake flow
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Flow-Induced Acoustic Resonances in Exhaust Gas Economizer Tube Banks 被引量:1
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作者 Satoru Okamoto 《Journal of Mechanics Engineering and Automation》 2013年第3期159-167,共9页
To investigate the conditions under which acoustic resonances occur, staggered arrays of closely spaced rigid tubes were tested in a wind tunnel under various flow velocities. The author investigated the Strouhal numb... To investigate the conditions under which acoustic resonances occur, staggered arrays of closely spaced rigid tubes were tested in a wind tunnel under various flow velocities. The author investigated the Strouhal numbers at which flow periodicities occur, the relation between these Strouhal numbers and those at which acoustic resonances occur, and the effects of Reynolds number and longitudinal tube spacings on the occurrence of acoustic resonance. This investigation showed the following: (1) Acoustic resonance can be produced at a frequency well removed from that of vortex shedding. The results also show evidence of vortex shedding and acoustic resonance existing simultaneously but at different frequencies. (2) Acoustic resonance behavior is consistent with that of a self-excited system. (3) A new model of this phenomenon provides an improved procedure for avoiding acoustic resonances in closely spaced tube banks. 展开更多
关键词 Flow-induced vibration flow measurements VORTEX aerodynamic acoustics resonance tube arrays.
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Experimental investigation on control of vortex shedding mode of a circular cylinder using synthetic jets placed at stagnation points 被引量:11
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作者 MA LiQun FENG LiHao 《Science China(Technological Sciences)》 SCIE EI CAS 2013年第1期158-170,共13页
Control of flow around a circular cylinder by synthetic jets has been experimentally investigated in a water tunnel with particle image velocimetry(PIV) technique.The synthetic jets are positioned at both the front an... Control of flow around a circular cylinder by synthetic jets has been experimentally investigated in a water tunnel with particle image velocimetry(PIV) technique.The synthetic jets are positioned at both the front and rear stagnation points.With power spectrum analysis,proper orthogonal decomposition(POD) method and other techniques for data processing,particular attention is paid to the control of vortical structures around the circular cylinder,in which the excitation frequency f e is one to three times of the natural frequency f0 and the cylinder Reynolds number and the excitation amplitude are fixed.The influenced-scope of the synthetic jet enlarges as the excitation frequency increases,and thus the synthetic jet dominates the global flow field gradually.For the natural case and the control case at fe/f0=1,the distributions of the first two POD modes and the power spectra for their POD coefficients all exhibit the characteristics of the natural shedding with antisymmetric mode.For fe/f0=2 and fe/f0=3,the variations in the third and fourth POD modes and the corresponding power spectra indicate that the wake vortex shedding mode changes and the dominant frequency becomes the excitation frequency.For fe/f0=2,the wake vortex sheds downstream with either the antisymmetric or the symmetric mode;for fe/f0=3,the synthetic jet vortex pair interacts with the near wake shear layers from both sides to induce a pair of the symmetric wake vortices,which is gradually converted into an antisymmetric mode when shedding downstream. 展开更多
关键词 flow control synthetic jet circular cylinder stagnation points wake vortex shedding mode
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