2022
DOI: 10.1016/j.tsep.2022.101296
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Numerical investigation of Thermo-aerodynamic characteristics of gas foil thrust bearing

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Cited by 7 publications
(1 citation statement)
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“…They found that cooling efficiency increases with increasing mass flowrate of the axial throughflow. Zhang et al [292] numerically verified that the heat generated by viscosity dissipation accounts for more than 90% of the aerodynamic heating of a gas foil thrust bearing. Such a large heat input cannot be neglected under working conditions at ultra-high rotation speeds.…”
Section: Management Of Thermal Effectsmentioning
confidence: 99%
“…They found that cooling efficiency increases with increasing mass flowrate of the axial throughflow. Zhang et al [292] numerically verified that the heat generated by viscosity dissipation accounts for more than 90% of the aerodynamic heating of a gas foil thrust bearing. Such a large heat input cannot be neglected under working conditions at ultra-high rotation speeds.…”
Section: Management Of Thermal Effectsmentioning
confidence: 99%