Performance simulation of multi-stage axial-flow compressor of turbo-shaft engine with account for erosive wear nonlinearity of its blades
The construction and useful practice of gas-turbine engine diagnosis systems depend largely on the availability of the engine mathematical models and its certain components in their structure. Utilization of multi-stage axial flow compressor performance with account for erosive wear of its parts dur...
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| פורמט: | Article |
| שפה: | Russian |
| יצא לאור: |
Moscow State Technical University of Civil Aviation
2020-10-01
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| סדרה: | Научный вестник МГТУ ГА |
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| גישה מקוונת: | https://avia.mstuca.ru/jour/article/view/1744 |