Stall Prediction in Gas-Turbine Engines
- 1 September 1959
- journal article
- Published by ASME International in Journal of Basic Engineering
- Vol. 81 (3) , 401-407
- https://doi.org/10.1115/1.4008487
Abstract
From a study of multistage compressors operating in gas-turbine engines the sequence of events which occur during the stall process was determined. By using this information and stage-characteristic curves, it is shown that the compressor stall limit may be computed for any disturbance.Keywords
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