Pages that link to "Item:Q2853486"
From MaRDI portal
The following pages link to Numerical investigation of mixing and combustion enhancement in supersonic combustors by strut induced streamwise vorticity (Q2853486):
Displaying 7 items.
- Numerical investigation on the flowfield of ``swallowtail'' cavity for supersonic mixing enhancement (Q362008) (← links)
- Study on main flow and fuel injector configurations for Scramjet applications (Q981504) (← links)
- Mixing characteristics in a supersonic combustor with gaseous fuel injection upstream of a cavity flameholder (Q1029619) (← links)
- Numerical study on supersonic combustion with cavity-based fuel injection (Q1434579) (← links)
- Assumed PDF Modeling of Turbulence Chemistry Interaction in Scramjet Combustors (Q5745263) (← links)
- Streamwise vortex breakdown due to the interaction with crossed shock waves (Q6080311) (← links)
- Investigation and assessment of production- and dissipation-limited DDES methods for rocket combustion chamber simulations (Q6566980) (← links)