NASA NTRS · 19840000168
Diverter Lip for Seal
Abstract
Proposed one-piece design change for cooling turbine rotor disks eliminates temperature differential that normally causes thermal stresses and cracks.
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Jackson, E. D., III, Johnson, D.. 1985-01-01. Diverter Lip for Seal. https://ntrs.nasa.gov/citations/19840000168
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