scholarly journals Numerical investigation of flows with condensation in micronozzles

2021 ◽  
Vol 2057 (1) ◽  
pp. 012016
Author(s):  
M A Korepanov ◽  
M R Koroleva ◽  
E A Mitrukova

Abstract The paper considers the numerical simulation of the flow of argon with account for the condensation process in the micronozzle and behind it. To describe phase transitions, the initial mathematical model of viscous heat-conducting gas flow is supplemented with the equation of formation and growth of condensation nuclei in the flow. The developed mathematical model allows for simulating the process of gas condensation at low pressures and temperatures. It is shown that the condensate mass fraction in the flow is not less than 1% at the pressure and temperature of 5 bar and 200 K, respectively, when argon flows out of a micronozzle to the environment with the pressure of 0.01 Pa. At the nozzle exit, the size of condensed particles reaches 80 angstroms. The obtained results confirm the necessity to take into account the condensation phenomenon in micronozzle flows of inert gases.

2017 ◽  
pp. 93-98
Author(s):  
D. D. Barannikova ◽  
A. G. Obukhov

The article analyzes experimental and analytical studies of ascending swirling air flows. In experimental works such flows are considered from the point of view of the direction of twist, the thermal regimes of heating the underlying surface, the estimation of integral parameters, the method of influence on them, and various methods of visualization. In analytical papers, by constructing solutions of the system of gas dynamics equations, the emergence of a twist of the corresponding direction is proven when there is a gas flow into a vertical cylinder of nonzero radius. In addition, in the numerical modeling of thermal ascending swirling flows, a feature was observed in the behavior of a moving gas at the initial moments of flow formation when the underlying surface was heated locally. This feature consists in the appearance on the boundary of the heating region of counter propagating gas flows with opposite directions of twist. The paper presents the results of numerical simulation of three-dimensional unsteady flows of a compressible viscous heat-conducting gas in thermal swirled vortices with local heating of the underlying surface, taking into account the action of gravity and Coriolis forces.


2019 ◽  
pp. 72-78
Author(s):  
Юрий Александрович Крашаница ◽  
Кристина Владимировна Гуторова

The current level of technological development is characterized by the constant complexity of the products. For its production requires processing a large number of parts of complex shape. Mathematical modeling is an effective and economical way to solve many technical problems. There are various ways to ensure the necessary cleanliness of machine parts or reduce the negative effects of technological pollution. Existing methods of finishing and cleaning parts on the physical-chemical effects on the material during processing are divided into several groups. The most widespread are both mechanical methods in which the removal of defects is carried out by mechanical action on machined parts of tools and chemical and mechanical methods in which there is a simultaneous mechanical effect of the tool and the chemical action of the external. The gas-dynamic method of removing defects that occur after the preliminary metalworking of parts of aircraft objects seems to be very effective. The mathematical model of this process is the system of laws for the conservation of the dynamics of a viscous heat-conducting gas, the physicochemical characteristics of which are established in an experimental way. The construction of a gas-dynamic model of the physical process of finishing parts as an arbitrary spatial form and the material of manufacture is presented. On the basis of the general laws of conservation of the dynamics of a viscous heat-conducting gas, analytical forms of solutions for the kinematic and dynamic characteristics of a high-temperature flow are obtained using the example of a flat channel simulating the surface of a part being cleaned. It is shown that in the flat case the conservation laws have a linear form, which provided exact solutions for the kinematic characteristics, such as the velocity and vorticity of a viscous gas flow, which play a major role in calculating the dynamic and thermal characteristics of the flow. The use of a generalized apparatus of vector-tensor analysis is fundamentally important in order to obtain integral representations of the solutions of differential forms of the laws of conservation of momentum and energy in the control region. Control of gas dynamic and thermodynamic parameters of the flow is able to provide a high-quality surface.


Author(s):  
Jiang Bian ◽  
Xuewen Cao

Abstract Condensation phenomenon has been studied actively for decades because of its extensive and significant applications in various fields of technology and engineering. The condensation phenomenon of condensable component in supersonic flows is still not understood very well as a result of the complex nucleation and droplet growth process, especially the condensation characteristic of gas mixture. In this paper, the Laval nozzle was designed based on the bi-cubic curve, state equation of real gas, arc plus straight line and viscous correction of boundary layer. The physical and mathematical models were developed to predict the condensation process in the supersonic air flows based on the nucleation and droplet growth theories, surface tension model and gas-liquid governing equations. The condensation processes of gaseous water/air binary (single condensable) gas and water/ethanol/air ternary (double condensable) gas mixture in the designed nozzle were simulated, and the reliability of the established models was verified by the experimental data. By comparing the condensation process of water/air binary gas with water/ethanol ternary gas, the influence of the second condensable component on the condensation process was analyzed. The results show that in the condensation process of gaseous water, as the pressure and temperature of water vapor decrease in the nozzle, spontaneous condensation occurs further downstream the nozzle throat. The nucleation rate grows rapidly from 0 to peak in a very short distance. With the consumption of water vapor, due to the decrease of the degree of supercooling, the nucleation environment is destroyed, and the nucleation rate quickly decreases to 0. The nucleation process is rapid in time and space, while the droplet growth process could maintain longer. The droplet number and mass fraction increase continuously till the nozzle outlet. There is a weak condensation in the nozzle due to the release of latent heat, but it is not obvious because the air acts as a heat container and absorbs the latent heat released by condensation. In the water/ethanol/air ternary system, the ethanol nucleates prior to water vapor. With the increase of supercooling, water vapor also begins to nucleate. In essence, there are two kinds of condensation nuclei (water nuclei and ethanol nuclei), and both the water and ethanol vapor can aggregate on these two kinds of condensation nuclei. Compared with the condensation process of water, the Wilson point of condensation is closer to the throat and the outlet mass fraction of liquid phase is greater in the condensation process of water/ethanol mixture, which shows that the water and ethanol can affect and promote each other. The maximum nucleation rate, droplet growth rate, droplet radius and outlet mass fraction of liquid phase of water/air binary and water/ethanol/air ternary mixture are about 9.46 × 1026 m−3s−1 and 2.57 × 1027 m−3s−1, 1.65 × 10−5 m/s and 1.02 × 10−5m/s, 1.32 × 10−7m and 1.63 × 10−7m, 0.19% and 1.34%, respectively.


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