Pages that link to "Item:Q2094182"
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The following pages link to 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):
Displaying 4 items.
- 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)
- 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)