Pages that link to "Item:Q969704"
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The following pages link to LES of a multi-burner annular gas turbine combustor (Q969704):
Displaying 11 items.
- Using LES to study reacting flows and instabilities in annular combustion chambers (Q431901) (← links)
- Study of flow and mixing in a generic GT combustor using LES (Q608130) (← links)
- LES to ease understanding of complex unsteady combustion features of ramjet burners (Q657623) (← links)
- Analysis of unsteady motion with respect to noise sources in a gas turbine combustor: isothermal flow case (Q853686) (← links)
- Experimental and computational investigations of flow and mixing in a single-annular combustor configuration (Q1037427) (← links)
- LES grid resolution requirements for the modelling of gravity currents (Q1615579) (← links)
- Large eddy simulation of the acoustic of a premixed swirl flame (Q1735011) (← links)
- Investigation of azimuthal staging concepts in annular gas turbines (Q3098132) (← links)
- Large eddy simulation modelling of combustion for propulsion applications (Q3559891) (← links)
- LES of jets in cross-flow and its application to a gas turbine burner (Q5942692) (← links)
- Robustness and reliability of state-space, frame-based modeling for thermoacoustics (Q6648375) (← links)