Small-scale dynamic structures in low-pressure microwave discharges

1997 ◽  
Vol 40 (8) ◽  
pp. 663-671 ◽  
Author(s):  
N. V. Vvedenskii ◽  
N. K. Vdovicheva ◽  
V. B. Gil’denburg ◽  
N. A. Zharova ◽  
I. A. Shereshevskii ◽  
...  
Author(s):  
Jeffery P. Bindon

The pressure distribution in the tip clearance region of a 2D turbine cascade was examined with reference to unknown factors which cause high heat transfer rates and burnout along the edge of the pressure surface of unshrouded cooled axial turbines. Using a special micro-tapping technique, the pressure along a very narrow strip of the blade edge was found to be 2.8 times lower than the cascade outlet pressure. This low pressure, coupled with a thin boundary layer due to the intense acceleration at gap entry, are believed to cause blade burnout. The flow phenomena causing the low pressure are of very small scale and do not appear to have been previously reported. The ultra low pressure is primarily caused by the sharp flow curvature demanded of the leakage flow at gap entry. The curvature is made more severe by the apparent attachement of the flow around the corner instead of immediately separating to increase the radius demanded of the flow. The low pressures are intensified by a depression in the suction corner and by the formation of a separation bubble in the clearance gap. The bubble creates a venturi action. The suction corner depression is due to the mainstream flow moving round the leakage and secondary vortices.


2018 ◽  
Vol 227 ◽  
pp. 672-685 ◽  
Author(s):  
M.A. Ancona ◽  
M. Bianchi ◽  
L. Branchini ◽  
A. De Pascale ◽  
F. Melino ◽  
...  

Energies ◽  
2019 ◽  
Vol 12 (23) ◽  
pp. 4512
Author(s):  
Michalina Kurkus-Gruszecka ◽  
Piotr Krawczyk

In the article the computational fluid dynamics (CFD) simulation and calculated operational parameters of the single stage low-pressure rotary lobe expander compared with the values obtained from a different geometry simulation are presented. Low-pressure rotary lobe expanders are rotary engines that use a compressed gas to produce mechanical energy, which in turn can be converted into another form, i.e., electric energy. Currently, expanders are used in narrow areas, but have a large potential in the energy production from gases of low thermodynamic parameters. The first geometry model was designed on the basis of an industrial device and validated with the empirical data. Simulation of the second geometry was made based on a validated model in order to estimate the operational parameters of the device. The CFD model included the transient simulation of compressible fluid in the geometry changing over time and the rotors motion around two rotation axes. The numerical model was implemented in ANSYS CFX software. After obtaining simulation results in the form of parameters monitors for each time step, a number of calculations were performed using a written code analysing the CFD program output files. The article presents the calculation results and the geometries comparison in terms of work efficiency. The research indicated that the construction of the device on a small scale could cause a significant decrease in the aforementioned parameter, caused by medium leaks in the expander clearances.


2000 ◽  
Vol 77 (18) ◽  
pp. 2825-2827 ◽  
Author(s):  
Tibor Terebessy ◽  
Masashi Kando ◽  
Jozef Kudela

1971 ◽  
Vol 10 (11) ◽  
pp. 2555 ◽  
Author(s):  
J. P. Campbell ◽  
E. W. Spisz ◽  
R. L. Bowman

1995 ◽  
Vol 74-75 ◽  
pp. 59-62 ◽  
Author(s):  
A. Ohl ◽  
H. Strobel ◽  
J. Röpcke ◽  
H. Kammerstetter ◽  
A. Pries ◽  
...  

Author(s):  
Roland Sigg ◽  
Timothy Rice

For flexible operation steam turbines may operate occasionally at low load. Operation away from the original design regime looks set to be an increasing trend mainly due to the presence of intermittently available renewable energy sources in the grid. This paper sets out an approach for considering low flow effects on turbine designs. At low load operating conditions rotating instabilities (RIS) can occur in the rear stages of LP steam turbines. The instabilities are comparable in many ways to rotating stall in compressors. Ideally the turbine blade natural frequencies should be designed to avoid the frequencies generated by the RIS system. The characteristics of RIS systems were experimentally investigated to understand the dependency with both flow coefficient and exhaust configuration. Correlations have been developed to characterize the dynamic pressure amplitudes and the fractional speed of the RIS moving around the wheel. The presented correlation based method is shown calibrated for a specific blade design. Two different test rigs provide the basis for the work presented. A low pressure model steam turbine provided detailed information for key blade/exhaust combinations. A simplified small scale air turbine was used to provide additional input for the behavior with alternative exhaust back wall position. Observations of the characteristic RIS behavior from model turbine tests are set in context with observed changes in the flow field.


Author(s):  
Jinbo Chen ◽  
Haiguang Gong ◽  
Lili Tong

An analytic investigation of the steam blocking in low pressure heating channels was conducted. In this paper, the dynamic model of the vapor-liquid interface is established through the basic conservation equations, and the rupture time of the vapor-liquid interface is predicted based on the Rayleigh-Taylor instability. Subsequently, the steam blocking model considering the steam accumulation and the vapor-liquid interface rupture in geysering flow is established. On these bases, the relative volume and relative pressure of the accumulated steam, the relative acceleration and perturbation intensity of the vapor-liquid interface, the time-varying behavior of the ratio of resistance and buoyancy are obtained. It is found that the accumulated steam basically increases linearly with the time going; The oscillation of the pressure and velocity, which is very large at the beginning time of the steam accumulation, decreases gradually with the continuous steam accumulation; The Reynolds number of the liquid within the rising section is very small at the stagnation state since there is no forced circulation flow, and finally a blockage is engendered in the pipeline with the steam accumulated. The theoretical results are in good agreements with the results obtained by a small-scale experiment. The mechanism model is able to predict the steam blocking property during the geysering flow in heating channels well, and can also establish a theoretical basis for the later analysis of the steam blocking elimination.


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