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Numerical computations of the unsteady flow in a radial turbine

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Numerical computations of the unsteady flow in a radial turbine ( numerical-computations-unsteady-flow-a-radial-turbine )

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3.4. TURBINE PERFORMANCE UNDER PULSATILE FLOW 23 an electrodynamic shaker. Tests were performed at two different frequencies of the pulsatile flow. Different phase settings between the pressure pulse and the movement of the nozzle were also tested. An increase in shaft power output with up to 7% was achieved with the active control system, but the efficiency was lower for the turbine fitted with this type of active control system. A better design is to active control the incidence angle of the vanes in a vaned nozzle. Rajoo & Martinez-Botas (2007) studied the performance of mixed flow turbines with moveable nozzle vanes. The movement of the nozzle vanes was controlled in both a passive way and in an active way with an actuator. In the passive system, an increasing pressure in the volute opened the vanes against a pre-loaded spring, and when the pressure decreased, the vanes were retracted. In this way, an increased area is obtained at high pressure, while the area is decreased at lower pressure. The passive system increased the shaft power output (with 36% for the best case) during the period of the pulse when the mass flow was low, but reduced the maximum power. The cycle averaged power was lower compared to a turbine with fixed vanes. Still the efficiency was better for the turbine with a passive control system. For the active system, with a forced movement of the vanes, a small improvement of the efficiency was achieved. The authors also concluded that of the tested control systems, a passive system with moveable nozzle vanes is probably the most beneficial system, especially for IC engines working with a narrow speed range. When computing the isentropic efficiency and U/Cs, it is common to as- sume that the pressure at the outlet of the turbine is constant during the pulse. This assumption can be doubted; special for small turbines with a size that is common for automotive applications. Capobianco & Marelli (2005) in- vestigated the unsteady pulsatile flow in a four to one exhaust manifold and a nozzle-less radial turbine, and one of the conclusions was that the flow un- steadiness at the turbine outlet cannot be neglected due to the fact that the measured pressure downstream of the turbine was not constant over a pulse period. The amplitude of the pressure variations was approximately 0.3 bar, and the amplitude of the pulse at the inlet to the turbine was for this case approximately 1.0 bar. The amplitude of the pressure variations downstream of the turbine also increased when the waste-gate valve was opened, since the maximum pressure before the turbine was higher, due to an increased mass flow through the system. Capobianco & Gambarotta (1990) also studied the effects of different waste-gate valve opening areas on the pressure pulses upstream and downstream of the turbine, and the results showed that the pressure pulses at the turbine inlet were unaffected by the waste-gate valve opening, while the pressure at the outlet of the turbine had a high frequency oscillation superim- posed. The frequency was about 3 kHz, but since neither the blade number nor the rotational speed of the wheel was specified in the report, no conclusion of

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