Pages that link to "Item:Q2094189"
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The following pages link to Rotating detonation combustor downstream transition passage design considerations (Q2094189):
Displaying 5 items.
- Parallel three-dimensional numerical simulation of rotating detonation engine on graphics processing units (Q1645599) (← links)
- Computational simulation of an exhaust plenum charged by a multi-tube pulsed detonation combustor (Q2094179) (← links)
- Pressure fluctuations in an annular plenum downstream of a multi-tube pulse detonation combustor (Q2094180) (← links)
- Numerical analysis of unsteady compressor performance under boundary conditions caused by pulsed detonation combustion (Q2094205) (← links)
- Development of a fast evaluation tool for rotating detonation combustors (Q2294811) (← links)