An ideal gas bulk flow model was established based on the two-control-volume isothermal bulk flow model developed by Kleynhans and Childs. A computational analysis was performed for prediction of the static and dynamic performance of gas annular hole-pattern seals at eccentric rotor conditions. The computational process was simplified by applying the perturbation method for small amplitude rotor excursion about an off-centered position. The flow field and rotordynamic coefficients were obtained by iteratively solving the simplified zeroth-order and first-order perturbation equations. The relations between the rotordynamic coefficients and excitation frequency were also calculated with the codes developed under different boundary conditions and geometrical sizes. The results obtained with the present method are well in agreement with the experimental data and more accurate than those with the isothermal bulk flow method. These findings confirm that the present method can be adopted to predict the rotordynamic characteristics of the hole-pattern seal.
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