Pages that link to "Item:Q1648228"
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The following pages link to Aerodynamic response of internal passages to pulsating inlet supersonic conditions (Q1648228):
Displaying 4 items.
- Hysteresis of shock wave locations in divergent bent channels (Q1735017) (← links)
- Rotating detonation combustor downstream transition passage design considerations (Q2094189) (← 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)