Separation control by a microfabricated SDBD plasma actuator for small engine turbine applications: influence of the excitation waveform

Author:

Pescini E.,De Giorgi M.G.,Suma A.,Francioso L.ORCID,Ficarella A.ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference56 articles.

1. Effects of input voltage on flow separation control for low-pressure turbine at low Reynolds number by plasma actuators;Matsunuma;Int. J. Rotating Mach.,2012

2. Predicting separation and transitional flow in turbine blades at low Reynolds numbers—part I: development of prediction methodology;Sanders;J. Turbomach.,2011

3. Unsteady flow field of an axial-flow turbine rotor at a low Reynolds number;Matsunuma;J. Turbomach.,2006

4. The fluid dynamics of LPT blade separation control using pulsed jets;Bons;J. Turbomach.,2002

5. J. Avinalexander, C. Sarojmala, M. Muthukumar, K. Kannamanimuthu, A.P. Haran, S. Soundaranayagam, Low Reynolds number performance of small engine turbine blade, in: 2nd International Conference on Innovative Research in Engineering and Technology, iCIRET2013, January 3–5, 2013.

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