Laboratory Investigations of a Low-Swirl Injector with H2 and CH4 at Gas Turbine Conditions

By R. Cheng. 2008

184 citations recorded by the source corpus.

Subfields: Computational Mechanics, Ocean Engineering

View Paper: https://www.semanticscholar.org/paper/c652afaa9c68cb8e195a0acedde9fb790ddb139a

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Computational Mechanics

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

In Ocean Engineering

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): “The LSI burner does not exhibit vortex breakdown with a central recirculation zone (CRZ) for flame stabilisation like conventional swirl-stabilised burners; rather the key aerodynamic feature for flame stabilisation is a non-swirling centre flow which inhibits vortex breakdown and promotes the forma”