Transient Calculation Studies of Liquid–Solid Collision in Jet Descaling
Abstract
:1. Introduction
2. Droplet–Scale Impact Model
2.1. Physical Analysis
2.2. Coupling of 2D Droplet–Scale Impact Model
2.3. Solving Droplet–Scale Impact Model
3. Simulation Results, Analysis, and Conclusions
Impact of the Droplet on the Scale
- The pressure value in the droplet keeps increasing. On the contact surface of the water droplet and the scale, the point of highest pressure always occurs at the edge of the interface (the shock front). Figure 3a–f clearly shows that the internal shock wavefront of the droplet forms a flat crown in the disturbance area. Because the density of water increases and the elastic modulus increases in the disturbed area, the speed of sound in the disturbed area is greater than that in the undisturbed area. Therefore, the pressure wave in the disturbed area can catch up with the initial pressure wavefront to form a superposition of the wavefront, thereby forming a shock wave.
- The pressure wave is transmitted faster in the radial direction than in the axial direction. Assuming a contact angle of θ, for a first-order approximation, the speed of motion at the contact edge point of the droplet with the scale is:For the collision process at the nanosecond level, if the impact velocity is considered constant, the equation is as follows:For r0 = 1 mm, v0 = 210 m/s, and t = 10 ns, the estimated moving speed of the edge point is ve = 3235 m/s, but the speed of sound in water is about 1430 m/s. At this time, the moving speed of the edge point is not only much greater than the impact speed but also greater than the speed of sound. Therefore, in the radial direction, the disturbance source moves faster than the speed of sound, but the pressure wave can only travel at the speed of sound. At this time, the maximum pressure point in the droplet appears inside the droplet. However, due to the lack of contact with the scale, it is not our main concern.
- Since the speed of sound in the scale (4268 m/s) is higher than the moving speed of the edge point, the propagation of the stress wave in the scale is less affected by the disturbance source, so the stress-wave influence area in the solid is spherical. There are two areas with high-stress values. The first is located near the edge of the water-droplet contact with the scale, which is where the peak pressure in the water droplet occurs. The second is located at a certain depth on the axis and is superimposed by the axially symmetrically distributed stress waves. This area is the source of stress at which scale erosion occurs at a certain depth.
4. Conclusions
Author Contributions
Funding
Data Availability Statement
Conflicts of Interest
References
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Scale | Droplet | |
---|---|---|
Density (m3/kg) | 4090 | 1000 |
Sonic speed (m/s) | 4268 | 1430 |
Acoustic impedance (kg/m2s) | 1.746 × 107 | 1.430 × 106 |
Young’s modulus (Pa) | 74.5 × 109 | |
Poisson’s ratio | 0.28 | |
Flexure (tensile) strength (MPa) | 75.4 | |
Compressive strength (MPa) | 1300 |
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Hu, S.; Teng, Z.; Huang, S.; Li, N.; Zhou, Q. Transient Calculation Studies of Liquid–Solid Collision in Jet Descaling. Energies 2023, 16, 292. https://doi.org/10.3390/en16010292
Hu S, Teng Z, Huang S, Li N, Zhou Q. Transient Calculation Studies of Liquid–Solid Collision in Jet Descaling. Energies. 2023; 16(1):292. https://doi.org/10.3390/en16010292
Chicago/Turabian StyleHu, Shu, Zhaohui Teng, Shan Huang, Na Li, and Qulan Zhou. 2023. "Transient Calculation Studies of Liquid–Solid Collision in Jet Descaling" Energies 16, no. 1: 292. https://doi.org/10.3390/en16010292
APA StyleHu, S., Teng, Z., Huang, S., Li, N., & Zhou, Q. (2023). Transient Calculation Studies of Liquid–Solid Collision in Jet Descaling. Energies, 16(1), 292. https://doi.org/10.3390/en16010292