NI, Dan ;YANG, Minguan ;GAO, Bo ;ZHANG, Ning ;LI, Zhong . Flow Unsteadiness and Pressure Pulsations in a Nuclear Reactor Coolant Pump. Strojniški vestnik - Journal of Mechanical Engineering, [S.l.], v. 62, n.4, p. 231-242, june 2018. ISSN 0039-2480. Available at: <https://www.sv-jme.eu/sl/article/flow-unsteadiness-and-pressure-pulsations-in-a-nuclear-reactor-coolant-pump/>. Date accessed: 19 nov. 2024. doi:http://dx.doi.org/10.5545/sv-jme.2015.3192.
Ni, D., Yang, M., Gao, B., Zhang, N., & Li, Z. (2016). Flow Unsteadiness and Pressure Pulsations in a Nuclear Reactor Coolant Pump. Strojniški vestnik - Journal of Mechanical Engineering, 62(4), 231-242. doi:http://dx.doi.org/10.5545/sv-jme.2015.3192
@article{sv-jmesv-jme.2015.3192, author = {Dan Ni and Minguan Yang and Bo Gao and Ning Zhang and Zhong Li}, title = {Flow Unsteadiness and Pressure Pulsations in a Nuclear Reactor Coolant Pump}, journal = {Strojniški vestnik - Journal of Mechanical Engineering}, volume = {62}, number = {4}, year = {2016}, keywords = {nuclear reactor coolant pump;flow unsteadiness;pressure pulsation;vorticity magnitude}, abstract = {Unsteady flow induced by rotor-stator interaction is detrimental to the safe operation of the nuclear reactor coolant pump, so it is essential to clarify flow structures and pressure pulsation in such pumps, especially within the spherical casing. In this paper, unsteady flow characteristics in a mixed-flow nuclear reactor coolant model pump were investigated using large-eddy simulation (LES) method. Results show that at the nominal flow rate, in two particular diffuser channels near the spherical casing discharge nozzle, the flow structures are uneven compared with that in the other flow channels. The reason is associated with the position of the flow channel with respect to the spherical casing nozzle. Large- scale flow separation and backflow structures easily occur at the regions near these two channels. In the right and the middle region of the casing nozzle, due to the large-scale separate flow and high vorticity magnitude, unsteady flow structures are more complicated in comparison with the other regions. It has been found that the vorticity spectra and the pressure spectra almost have the same main excitation frequencies. Therefore, it has been confirmed that for particular regions pressure pulsations are determined by the shedding vortex wake from the diffuser blade trailing edge of the nuclear reactor coolant model pump.}, issn = {0039-2480}, pages = {231-242}, doi = {10.5545/sv-jme.2015.3192}, url = {https://www.sv-jme.eu/sl/article/flow-unsteadiness-and-pressure-pulsations-in-a-nuclear-reactor-coolant-pump/} }
Ni, D.,Yang, M.,Gao, B.,Zhang, N.,Li, Z. 2016 June 62. Flow Unsteadiness and Pressure Pulsations in a Nuclear Reactor Coolant Pump. Strojniški vestnik - Journal of Mechanical Engineering. [Online] 62:4
%A Ni, Dan %A Yang, Minguan %A Gao, Bo %A Zhang, Ning %A Li, Zhong %D 2016 %T Flow Unsteadiness and Pressure Pulsations in a Nuclear Reactor Coolant Pump %B 2016 %9 nuclear reactor coolant pump;flow unsteadiness;pressure pulsation;vorticity magnitude %! Flow Unsteadiness and Pressure Pulsations in a Nuclear Reactor Coolant Pump %K nuclear reactor coolant pump;flow unsteadiness;pressure pulsation;vorticity magnitude %X Unsteady flow induced by rotor-stator interaction is detrimental to the safe operation of the nuclear reactor coolant pump, so it is essential to clarify flow structures and pressure pulsation in such pumps, especially within the spherical casing. In this paper, unsteady flow characteristics in a mixed-flow nuclear reactor coolant model pump were investigated using large-eddy simulation (LES) method. Results show that at the nominal flow rate, in two particular diffuser channels near the spherical casing discharge nozzle, the flow structures are uneven compared with that in the other flow channels. The reason is associated with the position of the flow channel with respect to the spherical casing nozzle. Large- scale flow separation and backflow structures easily occur at the regions near these two channels. In the right and the middle region of the casing nozzle, due to the large-scale separate flow and high vorticity magnitude, unsteady flow structures are more complicated in comparison with the other regions. It has been found that the vorticity spectra and the pressure spectra almost have the same main excitation frequencies. Therefore, it has been confirmed that for particular regions pressure pulsations are determined by the shedding vortex wake from the diffuser blade trailing edge of the nuclear reactor coolant model pump. %U https://www.sv-jme.eu/sl/article/flow-unsteadiness-and-pressure-pulsations-in-a-nuclear-reactor-coolant-pump/ %0 Journal Article %R 10.5545/sv-jme.2015.3192 %& 231 %P 12 %J Strojniški vestnik - Journal of Mechanical Engineering %V 62 %N 4 %@ 0039-2480 %8 2018-06-27 %7 2018-06-27
Ni, Dan, Minguan Yang, Bo Gao, Ning Zhang, & Zhong Li. "Flow Unsteadiness and Pressure Pulsations in a Nuclear Reactor Coolant Pump." Strojniški vestnik - Journal of Mechanical Engineering [Online], 62.4 (2016): 231-242. Web. 19 Nov. 2024
TY - JOUR AU - Ni, Dan AU - Yang, Minguan AU - Gao, Bo AU - Zhang, Ning AU - Li, Zhong PY - 2016 TI - Flow Unsteadiness and Pressure Pulsations in a Nuclear Reactor Coolant Pump JF - Strojniški vestnik - Journal of Mechanical Engineering DO - 10.5545/sv-jme.2015.3192 KW - nuclear reactor coolant pump;flow unsteadiness;pressure pulsation;vorticity magnitude N2 - Unsteady flow induced by rotor-stator interaction is detrimental to the safe operation of the nuclear reactor coolant pump, so it is essential to clarify flow structures and pressure pulsation in such pumps, especially within the spherical casing. In this paper, unsteady flow characteristics in a mixed-flow nuclear reactor coolant model pump were investigated using large-eddy simulation (LES) method. Results show that at the nominal flow rate, in two particular diffuser channels near the spherical casing discharge nozzle, the flow structures are uneven compared with that in the other flow channels. The reason is associated with the position of the flow channel with respect to the spherical casing nozzle. Large- scale flow separation and backflow structures easily occur at the regions near these two channels. In the right and the middle region of the casing nozzle, due to the large-scale separate flow and high vorticity magnitude, unsteady flow structures are more complicated in comparison with the other regions. It has been found that the vorticity spectra and the pressure spectra almost have the same main excitation frequencies. Therefore, it has been confirmed that for particular regions pressure pulsations are determined by the shedding vortex wake from the diffuser blade trailing edge of the nuclear reactor coolant model pump. UR - https://www.sv-jme.eu/sl/article/flow-unsteadiness-and-pressure-pulsations-in-a-nuclear-reactor-coolant-pump/
@article{{sv-jme}{sv-jme.2015.3192}, author = {Ni, D., Yang, M., Gao, B., Zhang, N., Li, Z.}, title = {Flow Unsteadiness and Pressure Pulsations in a Nuclear Reactor Coolant Pump}, journal = {Strojniški vestnik - Journal of Mechanical Engineering}, volume = {62}, number = {4}, year = {2016}, doi = {10.5545/sv-jme.2015.3192}, url = {https://www.sv-jme.eu/sl/article/flow-unsteadiness-and-pressure-pulsations-in-a-nuclear-reactor-coolant-pump/} }
TY - JOUR AU - Ni, Dan AU - Yang, Minguan AU - Gao, Bo AU - Zhang, Ning AU - Li, Zhong PY - 2018/06/27 TI - Flow Unsteadiness and Pressure Pulsations in a Nuclear Reactor Coolant Pump JF - Strojniški vestnik - Journal of Mechanical Engineering; Vol 62, No 4 (2016): Strojniški vestnik - Journal of Mechanical Engineering DO - 10.5545/sv-jme.2015.3192 KW - nuclear reactor coolant pump,flow unsteadiness,pressure pulsation,vorticity magnitude N2 - Unsteady flow induced by rotor-stator interaction is detrimental to the safe operation of the nuclear reactor coolant pump, so it is essential to clarify flow structures and pressure pulsation in such pumps, especially within the spherical casing. In this paper, unsteady flow characteristics in a mixed-flow nuclear reactor coolant model pump were investigated using large-eddy simulation (LES) method. Results show that at the nominal flow rate, in two particular diffuser channels near the spherical casing discharge nozzle, the flow structures are uneven compared with that in the other flow channels. The reason is associated with the position of the flow channel with respect to the spherical casing nozzle. Large- scale flow separation and backflow structures easily occur at the regions near these two channels. In the right and the middle region of the casing nozzle, due to the large-scale separate flow and high vorticity magnitude, unsteady flow structures are more complicated in comparison with the other regions. It has been found that the vorticity spectra and the pressure spectra almost have the same main excitation frequencies. Therefore, it has been confirmed that for particular regions pressure pulsations are determined by the shedding vortex wake from the diffuser blade trailing edge of the nuclear reactor coolant model pump. UR - https://www.sv-jme.eu/sl/article/flow-unsteadiness-and-pressure-pulsations-in-a-nuclear-reactor-coolant-pump/
Ni, Dan, Yang, Minguan, Gao, Bo, Zhang, Ning, AND Li, Zhong. "Flow Unsteadiness and Pressure Pulsations in a Nuclear Reactor Coolant Pump" Strojniški vestnik - Journal of Mechanical Engineering [Online], Volume 62 Number 4 (27 June 2018)
Strojniški vestnik - Journal of Mechanical Engineering 62(2016)4, 231-242
© The Authors, CC-BY 4.0 Int. Change in copyright policy from 2022, Jan 1st.
Unsteady flow induced by rotor-stator interaction is detrimental to the safe operation of the nuclear reactor coolant pump, so it is essential to clarify flow structures and pressure pulsation in such pumps, especially within the spherical casing. In this paper, unsteady flow characteristics in a mixed-flow nuclear reactor coolant model pump were investigated using large-eddy simulation (LES) method. Results show that at the nominal flow rate, in two particular diffuser channels near the spherical casing discharge nozzle, the flow structures are uneven compared with that in the other flow channels. The reason is associated with the position of the flow channel with respect to the spherical casing nozzle. Large- scale flow separation and backflow structures easily occur at the regions near these two channels. In the right and the middle region of the casing nozzle, due to the large-scale separate flow and high vorticity magnitude, unsteady flow structures are more complicated in comparison with the other regions. It has been found that the vorticity spectra and the pressure spectra almost have the same main excitation frequencies. Therefore, it has been confirmed that for particular regions pressure pulsations are determined by the shedding vortex wake from the diffuser blade trailing edge of the nuclear reactor coolant model pump.