Rotating stall

In a method of numerical modelling of the operation of a gas turbine engine (10), randomly chosen numerical modifications are made to values within the model, to represent a disturbance for triggering rotating stall. This results in a faster onset of rotating stall within the model, reducing the com...

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Bibliographische Detailangaben
Hauptverfasser: VAHDATI, MEHDI, SAYMA, NASER, IMREGUN, MEHMET
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:In a method of numerical modelling of the operation of a gas turbine engine (10), randomly chosen numerical modifications are made to values within the model, to represent a disturbance for triggering rotating stall. This results in a faster onset of rotating stall within the model, reducing the computational effort required to achieve this.