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Three-step approach for prediction of limit cycle pressure oscillations in combustion chambers of gas turbines - MaRDI portal

Three-step approach for prediction of limit cycle pressure oscillations in combustion chambers of gas turbines (Q5073622)

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scientific article; zbMATH DE number 7516716
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Three-step approach for prediction of limit cycle pressure oscillations in combustion chambers of gas turbines
scientific article; zbMATH DE number 7516716

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    Three-step approach for prediction of limit cycle pressure oscillations in combustion chambers of gas turbines (English)
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    3 May 2022
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    combustion instabilities
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    limit cycle
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    time-domain simulations
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    URANS
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    FSC model
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