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Dtic Adp011172%3a Active Control Of Combustion Instabilities In Gas Turbine Engines For Low Emissions. Part I%3a Physics Based And Experimentally Identified Models Of Combustion Instability by Defense Technical Information Center

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1DTIC ADP011172: Active Control Of Combustion Instabilities In Gas Turbine Engines For Low Emissions. Part I: Physics-Based And Experimentally Identified Models Of Combustion Instability

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This paper details the development of a thermoacoustic model and associated dynamic analysis. The model describes the results obtained in a gas fueled experimental combustion program carried out at UTRC. The contents of the paper are (a) the development of a thermoacoustic model composed of acoustic and heat release components, (b) the dynamic analysis of the resulting non-linear model using harmonic balance methods to compute linear stability boundaries and the amplitudes of oscillations and (c) the calibration of the model to experimental data.

“DTIC ADP011172: Active Control Of Combustion Instabilities In Gas Turbine Engines For Low Emissions. Part I: Physics-Based And Experimentally Identified Models Of Combustion Instability” Metadata:

  • Title: ➤  DTIC ADP011172: Active Control Of Combustion Instabilities In Gas Turbine Engines For Low Emissions. Part I: Physics-Based And Experimentally Identified Models Of Combustion Instability
  • Author: ➤  
  • Language: English

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The book is available for download in "texts" format, the size of the file-s is: 12.80 Mbs, the file-s for this book were downloaded 110 times, the file-s went public at Sat Oct 31 2015.

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