Pages that link to "Item:Q412814"
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The following pages link to Numerical research on mixing characteristics of different injection schemes for supersonic transverse jet (Q412814):
Displaying 10 items.
- Flowfield characteristics on a vent slot mixer in supersonic flow (Q358597) (← links)
- Numerical study of the injection process in a transonic wind tunnel. II: The off-design points (Q435316) (← links)
- Numerical study of spatial supersonic flow of a perfect gas with transverse injection of jets (Q468811) (← 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)
- Overset structured grids assembly method for numerical simulations of multi-bodies and moving objects (Q1615633) (← links)
- Numerical investigation of flow field effects on fuel-air mixing in a non-reacting trapped vortex combustor with different injection arrangements (Q2183837) (← links)
- Investigation of possibly variation of aerodynamic parameters for systems with injections with the help of a mathematical modeling method (Q2737291) (← links)
- Application and theoretical analysis of the flamelet model for supersonic turbulent combustion flows in the scramjet engine (Q5071068) (← links)
- Predictions of axial and transverse injection into supersonic flow (Q5952017) (← links)