By Rudibert King
The publication experiences at the newest theoretical and experimental advances within the box of energetic movement and combustion keep an eye on. It covers new advancements in actuator expertise and sensing, in strong and optimum open- and closed-loop regulate, in addition to in version aid for keep an eye on. It collects contributions awarded throughout the 3rd version of the lively move and Combustion keep watch over convention, held in September 10-12, 2014 on the Technische Universität Berlin (Germany). This convention, in addition to the examine offered within the publication, were supported by means of the collaborative learn heart SFB 1029 -Substantial potency elevate in gasoline generators via direct use of coupled unsteady combustion and movement dynamics, funded via the DFG (German examine Foundation).
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Extra resources for Active Flow and Combustion Control 2014
Annu. Rev. Fluid Mech. 43, 247–272 (2011) 7. : The Control of Flow Separation by Periodic Excitation. Progress in Aerospace Sciences 36, 487–545 (2000) 8. : Loss Reduction in Compressor Cascades by Means of Passive Flow Control. In: ASME Turbo Expo. (2008) 9. : Experimental and numerical results of active ﬂow control on a highly loaded stator cascade. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy 225, 907–918 (2011) 10. : Experimental AFC Approaches on a Highly Loaded Compressor Cascade.
Active Boundary Layer Control with Fluidic Oscillators 21 Nomenclature cp F p l m Ma R dimensionless pressure coefficient, eq. (1) and specific heat at constant pressure frequency (static) pressure chord length mass flow Mach number pressure ratio, eq. (4) Re t T Tu u x γ ζ Reynolds number pitch total temperature turbulence intensity pitchwise direction coordinate in axial direction specific heat ratio loss coefficient, eq. (2) integral loss coefficient ref t th reference condition total or stagnation condition theoretical value, based on no loss in cascade Subcripts 1 2 k NA pl plane upstream of cascade plane downstream of cascade pressure tank value no activation actuator plenum value Abbreviations blc LPT boundary layer control Low Pressure Turbine HGK high speed cascade wind tunnel References 1.
Section 2 brieﬂy reviews ILC and RC. Section 3 describes the compressor stator cascade in detail and Sec. 4 introduces the surrogate control variable and the control architecture. Experimental closed-loop results are presented in Sec. 5 and in Sec. 6 a conclusion is drawn. e. optimisation based ILC  and H∞ –optimal RC , are revisited in this section. Whereas a time-domain description will be given for ILC, frequency-domain approaches will be better suited for RC. 1 Iterative Learning Control System Description.