MS, University of Cincinnati, 2016, Engineering and Applied Science: Mechanical Engineering
Squeeze-film dampers (SFDs) are commonly used in aircraft engines because of their high damping coefficient and the associated ability to dissipate vibrations and improve the dynamic stability of rotor-bearing systems. The goal of the present work is to perform Computational Fluid Dynamics (CFD) simulation of uncavitated, end-sealed SFDs with axially centered or offset circumferential groove, and compare the simulation results for the tangential and radial forces with experimental data. For circular whirling motion of the SFD, a moving reference frame (MRF) formulation is used to transform the otherwise time-varying fluid domain to a time-independent domain, and enable an efficient steady-state simulation. The approach is first verified by comparing the simulation results with the Reynolds analytical solutions for long SFD (wherein pressure is a function of only the azimuthal direction, &theta) and short SFD (wherein pressure is a function of both &theta and the axial direction, z) bearings. The Reynolds solutions neglect inertia (Reynolds number Re = 0), whereas the computational model requires a non-zero Re, howsoever small. With Re = 0.96, the computed tangential force (directly proportional to damping) yields just 0.09% and 0.66% difference for the long and short SFD Reynolds solutions, respectively, thereby verifying the correct implementation of the MRF formulation. Next, the mathematical model used is validated by comparing the CFD results with available experimental data. The computed tangential force for the centered- and offset-groove configurations compares within 6.55% and 6.72%, respectively, with the data, suggesting that the simulation methodology developed can be used, within this tolerance, to predict the forces for end-sealed SFDs. Finally, a parametric study is conducted by varying geometrical parameters (radial clearance and groove position) and operating parameters (feeding pressure, feeding temperature, and whirling speed) for this flow. Groov (open full item for complete abstract)
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Committee: Urmila Ghia Ph.D. (Committee Chair); Kirti Ghia Ph.D. (Committee Member); Jay Kim Ph.D. (Committee Member)
Subjects: Mechanical Engineering