Attenuation of Gas Turbine Combustor Pressure Oscillations Using Symmetry Breaking
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
2011-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
ATTENUATION OF GAS TURBINE COMBUSTOR PRESSURE OSCILLATIONS USING SYMMETRY BREAKING
British Library Conference Proceedings | 2011
|Statistical characteristics of pressure oscillations in a premixed combustor
Online Contents | 2003
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