By Rudibert King
The ebook reviews at the most modern theoretical and experimental advances within the box of energetic circulation and combustion regulate. It covers new advancements in actuator know-how and sensing, in powerful and optimum open- and closed-loop regulate, in addition to in version aid for keep an eye on. It collects contributions offered throughout the 3rd variation of the lively stream and Combustion keep watch over convention, held in September 10-12, 2014 on the Technische Universität Berlin (Germany). This convention, in addition to the learn offered within the ebook, were supported by means of the collaborative examine heart SFB 1029 -Substantial potency elevate in fuel generators via direct use of coupled unsteady combustion and move dynamics, funded by way of the DFG (German learn Foundation).
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Extra info for Active Flow and Combustion Control 2014
10. Concerning the 2-norm of the error of one iteration eTi ei , the ILC performs better than the RC, see Fig. 10 (left). Regarding the progress of the control error during one iteration, see Fig. e. 21 s]. This is due to the fact that the sidewall actuation device can only blow but not suck, see Fig. 10 (right, bottom). e. 5 s], both controllers perform well. However, the RC reacts more aggressively to non-periodic disturbances. This is not beneﬁcial, since it often results in less favourable initial conditions for the next iteration.
Sure side The RM S(cp ) distribution indicates an upstream shift of the LSB at a certain phase angle to s/S = 23%. It is not only the position of the LSB which is inﬂuenced by the periodical choking, but along with it also the corner vortex breakdown. The position of the corner vortex breakdown is still s/S = 30% and in time-averaged data higher blocking of the passage leads to an earlier ﬂow separation resulting in a lower static pressure rise of the choked passage. The analysis of the blades pressure side is shown in Figure 5.
ASME Paper 2000GT-268 (2000) 6. : The Application of Ultra High Lift Blading in the BR 715 LP Turbine. ASME J. Turbomach. 124, 45–51 (2002) 7. : On the Impact of Blade Count Reduction on Aerodynamic Performance and Loss Generation in a Three-Stage LP Turbine. ASME Paper 2001-GT-0197 (2001) 8. : Aerodynamic Design of Low-Pressure Turbines, AGARD Lecture Series No. 167 (1989) 9. : A Comparison of Three Low Pressure Turbine Designs. ASME J. Turbomach. 135, 051026 (2013) 22 R. Niehuis and M. Mack 10.
Active Flow and Combustion Control 2014 by Rudibert King