Pages that link to "Item:Q2094205"
From MaRDI portal
The following pages link to Numerical analysis of unsteady compressor performance under boundary conditions caused by pulsed detonation combustion (Q2094205):
Displaying 7 items.
- Effects of pulse flow and leading edge sweep on mixed flow turbines for engine exhaust heat recovery (Q546565) (← links)
- Pressure fluctuations in an annular plenum downstream of a multi-tube pulse detonation combustor (Q2094180) (← links)
- Reduction of pressure fluctuations in an annular pulsed detonation combustor mockup by iterative learning control using eigenvector-based binary solution sets and iterative model identification (Q2094182) (← links)
- Rotating detonation combustor downstream transition passage design considerations (Q2094189) (← links)
- Efficiency increase and start-up strategy of an axial turbine stage under periodic inflow conditions using extremum seeking control (Q2094206) (← links)
- A comparison of optimal, binary closed-loop active flow control applied to an annular compressor stator cascade with periodic disturbances (Q2094209) (← links)
- An integrated modeling approach for variable cycle engine performance analysis (Q6157318) (← links)
