Pages that link to "Item:Q431901"
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The following pages link to Using LES to study reacting flows and instabilities in annular combustion chambers (Q431901):
Displaying 12 items.
- 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)
- The swept rule for breaking the latency barrier in time advancing PDEs (Q729369) (← links)
- Comparative study of coupling coefficients in Dirichlet-Robin procedure for fluid-structure aerothermal simulations (Q729533) (← links)
- LES of a multi-burner annular gas turbine combustor (Q969704) (← links)
- Experimental and computational investigations of flow and mixing in a single-annular combustor configuration (Q1037427) (← links)
- Representing the geometrical complexity of liners and boundaries in low-order modeling for thermoacoustic instabilities (Q2128354) (← links)
- Large-eddy simulations of unsteady hydrogen annular flames (Q2446664) (← links)
- A nonlinear model for indirect combustion noise through a compact nozzle (Q2878399) (← links)
- Large eddy simulation modelling of combustion for propulsion applications (Q3559891) (← links)
- An analytical study of the flame dynamics of a transversely forced asymmetric two-dimensional Bunsen flame (Q5073607) (← links)
- Acoustic modal analysis with heat release fluctuations using nonlinear eigensolvers (Q6096386) (← links)