This paper presents an improved dynamic analysis for liquid annular se
als with arbitrary profile based on a method first proposed by Nelson
and Nguyen. An improved first-order solution that incorporates a conti
nuous interpolation of perturbed quantities in the circumferential dir
ection is presented. The original method uses an approximation scheme
for circumferential gradients of zeroth order solution based on Fast F
ourier Transforms (FFT). A simpler scheme based on cubic splines is fo
und to be computationally more efficient, with better convergence at h
igher eccentricities. Arbitrarily varying seal profiles in both axial
and circumferential directions are considered. A procedure for computi
ng dynamic coefficients based on external specific load is discussed.
An example case of an elliptical seal with varying degrees of axial cu
rvature is analyzed. A case study based on actual operating clearances
(6 axial planes with 68 clearances/plane) of an interstage seal of th
e Space Shuttle Main Engine High Pressure Oxygen Turbopump (SSME-ATD-H
POTP) is presented.