Gas turbine shaft over-speed / failure modelling: aero/thermodynamics modelling and overall engine system response
Gas turbine design needs of high-speed turbomachinery whose layout is organised in compressor-turbine pairs mechanically linked by concentric shafts. The mechanical failure of a shaft leads to compressor-turbine decoupling provoking the acceleration of the free-running turbine. In view of such scena...
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| Language: | en |
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Cranfield University
2017
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| Online Access: | http://dspace.lib.cranfield.ac.uk/handle/1826/12131 |