Pages that link to "Item:Q617232"
From MaRDI portal
The following pages link to A numerical study of turbulent combustion characteristics in a combustion chamber of a scramjet engine (Q617232):
Displaying 12 items.
- Numerical research on mixing characteristics of different injection schemes for supersonic transverse jet (Q412814) (← links)
- Interface delamination of the thermal barrier coating subjected to local heating (Q546450) (← links)
- A flamelet model for turbulent diffusion combustion in supersonic flow (Q546460) (← links)
- Numerical investigation of the ramjet and scramjet operation regimes of the HIFiRE-2 combustion chamber (Q2107833) (← links)
- Effect of turbulence model uncertainty on scramjet strut injector flow field analysis (Q2245527) (← links)
- Highly-resolved large-eddy simulations of combustion stabilization in a scramjet engine model with cavity flameholder (Q2285517) (← links)
- Simulation of turbulent combustion in DLR scramjet (Q2644636) (← links)
- Influence of reaction mechanisms, grid spacing, and inflow conditions on the numerical simulation of lifted supersonic flames (Q3552152) (← links)
- Numerical investigation of turbulent hydrogen combustion in a SCRAMJET using flamelet modeling (Q4528439) (← links)
- Application and theoretical analysis of the flamelet model for supersonic turbulent combustion flows in the scramjet engine (Q5071068) (← links)
- Air Chemical Non-Equilibrium Effects on the Hypersonic Combustion Flow of RCS with Gaseous Ethylene Fuel (Q5156617) (← links)
- A correction for Reynolds-averaged-Navier-Stokes turbulence model under the effect of shock waves in hypersonic flows (Q6537418) (← links)
