Active Flow and Combustion Control 2014 by Rudibert King PDF

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By Rudibert King

ISBN-10: 3319119664

ISBN-13: 9783319119663

ISBN-10: 3319119672

ISBN-13: 9783319119670

The e-book reviews at the most up-to-date theoretical and experimental advances within the box of lively move and combustion regulate. It covers new advancements in actuator expertise and sensing, in powerful and optimum open- and closed-loop keep watch over, in addition to in version aid for keep watch over. It collects contributions awarded in the course of the 3rd version of the energetic move and Combustion regulate convention, held in September 10-12, 2014 on the Technische Universität Berlin (Germany). This convention, in addition to the examine offered within the booklet, were supported by way of the collaborative learn heart SFB 1029 -Substantial potency bring up in gasoline generators via direct use of coupled unsteady combustion and circulate dynamics, funded by way of the DFG (German learn Foundation).

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Extra resources for Active Flow and Combustion Control 2014

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93% case shows a much more increasing pressure coefficient until reaching x/L = 80%, from where it stays at a constant level. It follows that the AFC has an impact on the pressure side as well. Using AFC 36 M. Staats, W. Nitsche, and I. Peltzer along the whole blade a pressure rise on the pressure side can be observed. The positive area between the suction- and the pressure surface Δcp distribution indicates the benefit of the operating range of the stator due to the actuation. 5 Conclusion and Outlook Within the Collaborative Research Centre 1029 a highly loaded linear compressor cascade is used, with major three-dimensional flow structures and a trailing edge separation under design conditions causing high losses without AFC.

71·L P v1 (a) cascade (b) measurement blade Fig. 1. Experimental setup AFC on a Highly Loaded Compressor Cascade 25 rig, thus causing a maximum periodical wake blocking of 90% for any one passage, which results in a 13% all time blocking of the whole cascade wake area. The blade movements are described by a sinus motion and result in a passage blocking, which is shown in Figure 2a as a function of the phase angle for three passages. Passage three represents the passage on the pressure side of the measurement blade and passage five the one next to the measurement passage.

4. Time-averaged flow structure on suction side 28 M. Staats, W. Nitsche, and I. Peltzer The baseflow is well documented in [12]. Comparing the fundamental flow structures of the choked case with the  baseflow leads to the conclusion that   the size of the LSB becomes larger   in the choked case. The periodical   choking influences the inflow condi  tion in a way that the Reynolds num  ber changes periodically. This affects    the position of the LSB and causes it to oscillate in respect of the phase     angle of the choking apparatus.

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Active Flow and Combustion Control 2014 by Rudibert King


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