Flame macrostructures, combustion instability and extinction strain scaling in swirl-stabilized premixed CH4/H2 combustion

By Santosh Shanbhogue, Y. Sanusi, Soufien Taamallah, M. Habib, E. Mokheimer, Ahmed F. Ghoniem. 2016

205 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Fluid Flow and Transfer Processes

View Paper: https://www.semanticscholar.org/paper/86f0be4e29fba178988345bb9c7e2b4e9539d990

How researchers see this paper

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In Aerospace Engineering

1. Jadeed Beita
2. R. Balachandran
3. M. Talibi
4. S. Sadasivuni

In Computational Mechanics

1. Jadeed Beita
2. R. Balachandran
3. M. Talibi
4. S. Sadasivuni

In Fluid Flow and Transfer Processes

1. Jadeed Beita
2. R. Balachandran
3. M. Talibi
4. S. Sadasivuni

Citations in the corpus

• Thermoacoustic Instability Considerations for High Hydrogen Combustion in Lean Premixed Gas Turbine Combustors: A Review (2021, background): “[75] demonstrated that the higher extinction strain rates of the high hydrogen mixtures was the enabling mechanism which allowed the flame to penetrate into the ORZ and stabilise at lower equivalence ratios compared to pure methane, hence the reason for the flame shape transitions at lower equivalen”