GAS TURBINE COMBUSTION—Alternative Fuels and Emissions
By A. Lefebvre, D. R. Ballal, D. Bahr. 2010
749 citations recorded by the source corpus.
Subfields: Computational Mechanics, Electrical and Electronic Engineering, Fluid Flow and Transfer Processes
View Paper: https://www.semanticscholar.org/paper/3ee6c6b2357c05a794c3be424347ea9b891d77b3
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In Computational Mechanics
In Fluid Flow and Transfer Processes
Citations in the corpus
- Thermoacoustic Instability Considerations for High Hydrogen Combustion in Lean Premixed Gas Turbine Combustors: A Review (2021, background): “This results in substantial reduction in acoustic damping in contrast to diffusion-flame combustors where secondary and dilution air provide excellent sound attenuation [20,22].”
- Advances in rapid compression machine studies of low- and intermediate-temperature autoignition phenomena (2017, neutral): “Current gas turbines for power production typically operate at pressure ratios between 15–30, and aeroengine turbines operate at pressure ratios around 40–45 [28].”