An efficient algorithm for blade loss simulations applied to a high-order rotor dynamics problem
In this thesis, a novel approach is presented for blade loss simulation of an aircraft gas turbine rotor mounted on rolling element bearings with squeeze film dampers, seal rub and enclosed in a flexible housing. The modal truncation augmentation (MTA) method provides an efficient tool for modeling...
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| Format: | Others |
| Language: | en_US |
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Texas A&M University
2004
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| Online Access: | http://hdl.handle.net/1969.1/189 |