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Application of an improved Nelson-Nguyen analysis to eccentric, arbitrary profile liquid annular sealsAn improved dynamic analysis for liquid annular seals with arbitrary profile based on a method, first proposed by Nelson and Nguyen, is presented. An improved first order solution that incorporates a continuous interpolation of perturbed quantities in the circumferential direction, is presented. The original method uses an approximation scheme for circumferential gradients, based on Fast Fourier Transforms (FFT). A simpler scheme based on cubic splines is found to be computationally more efficient with better convergence at higher eccentricities. A new approach of computing dynamic coefficients based on external specified load is introduced. This improved analysis is extended to account for arbitrarily varying seal profile in both axial and circumferential directions. An example case of an elliptical seal with varying degrees of axial curvature is analyzed. A case study based on actual operating clearances of an interstage seal of the Space Shuttle Main Engine High Pressure Oxygen Turbopump is presented.
Document ID
19940029676
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Padavala, Satyasrinivas
(Texas A&M Univ. College Station., United States)
Palazzolo, Alan B.
(Texas A&M Univ. College Station., United States)
Vallely, Pat
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Ryan, Steve
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Publication Information
Publication: NASA. Lewis Research Center, Rotordynamic Instability Problems in High-Performance Turbomachinery, 1993
Subject Category
Mechanical Engineering
Accession Number
94N34182
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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