NASA NTRS · 19880000440
Seals For Cryogenic Turbomachines
Abstract
Analysis considers effects of seals on stability. Report presents method of calculation of flows of cryogenic fluids through shaft seals. Key to stability is local average velocity in seal. Local average velocity strongly influenced by effects of inlet and outlet and injection of fluid.
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Hendricks, Robert C., Tam, L. T., Braun, M. J., Vlcek, B. L.. 1988-09-01. Seals For Cryogenic Turbomachines. https://ntrs.nasa.gov/citations/19880000440
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