Browsing Centre for Product Design and Manufacturing (CPDM) by Subject "Jet Engine Compressor Blades"
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Prediction of Physical Behavior of Rotating Blades under Tip-Rub Impact using Numerical Modeling
(2018-02-09)Rotating blades, which are the most critical components of any turbo-machinery, need to be designed to withstand forced vibrations due to accidental tip rub impact against inner surface of casing. These vibrations are ...