Effect of Unsteady Wake on Flow Control of the Low-Pressure High-Lift Cascade with Synthetic Jet

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Abstract:

The flow separation is susceptible to appear and is known to affect the aerodynamic performance of the low-pressure high-lift cascade. Large Eddy Simulation was adopted in the present work and the periodic moving bar was employed to simulate the unsteady wake upstream of the blade. The flow control of the synthetic jet with unsteady wake was investigated in detail. The upstream wake increased the turbulent level of the boundary layer of the cascade. The synthetic jet got a better control under the effect of the upstream wake.

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Periodical:

Advanced Materials Research (Volumes 588-589)

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1790-1793

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November 2012

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© 2012 Trans Tech Publications Ltd. All Rights Reserved

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[1] D. You, P. Moin: Journal of Fluids and Structures, Vol. 24 (2008) No. 8, p.1349.

Google Scholar

[2] Y.B. Suzen, P.G. Huang: Journal of Turbomachinery, Vol 127 (2005) No. 3, p.431.

Google Scholar

[3] J. Smagorinsky: Monthly Weather Review, Vol 91 (1963) No. 3, p.99.

Google Scholar

[4] K. Matsuura, C. Kato: AIAA Journal, Vol 45 (2007) No. 2, p.442.

Google Scholar

[5] J.F. Donovan, L.D. Kral, A.W. Cary: 36th Aerospace Sciences Meeting and Exhibit (Reno, Nevada, USA, January 12-15, 1998). AIAA-1998-210.

DOI: 10.2514/6.1998-210

Google Scholar

[6] F.R. Menter: AIAA Journal, Vol 32 (1994) No. 8, p.1598.

Google Scholar

[7] H.P. Hodson, R.J. Howell: Annual Review of Fluid Mechanics, Vol 37 (2005), p.71.

Google Scholar