Effects of the Actuation on the Boundary Layer of an Airfoil at Reynolds Number Re = 60000-Reference-Cited by-同舟云学术

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Effects of the Actuation on the Boundary Layer of an Airfoil at Reynolds Number Re = 60000

Published:2020-05-29 Issue:2 Volume:105 Page:607-626
ISSN:1386-6184
Container-title:Flow, Turbulence and Combustion
language:en
Short-container-title:Flow Turbulence Combust

Author:

Rodriguez Ivette,Lehmkuhl Oriol,Borrell Ricard

Funder

Ministerio de Economía y Competitividad, Gobierno de España

Horizon 2020 Framework Programme

European Research Council

Publisher

Springer Science and Business Media LLC

Subject

Physical and Theoretical Chemistry,General Physics and Astronomy,General Chemical Engineering

Link

https://link.springer.com/content/pdf/10.1007/s10494-020-00160-y.pdf

Reference48 articles.

1. Akbarzadeh, A., Borazjani, I.: A numerical study on controlling flow separation via surface morphing in the form of backward traveling waves. In: AIAA Aviation Forum, pp. 1–11 (2019)

2. Alam, M., Sandham, N.: Direct numerical simulation of short separation bubbles with turbulent reattachment. J. Fluid Mech. 410, 1–28 (2000)

3. Albers, M., Meysonnat, P.S., Schröder, W.: Actively reduced airfoil drag by transversal surface waves. Flow Turbul. Combust. 102(4), 865–886 (2019)

4. Amitay, M., Glezer, A.: Role of actuation frequency in controlled flow reattachment over a stalled airfoil. AIAA J. 40(2), 209–216 (2002)

5. Amitay, M., Smith, D.R., Kibens, V., Parekh, D.E., Glezer, A.: Aerodynamic flow control over an unconventional airfoil using synthetic jet actuators. AIAA J. 39(3), 361–370 (2001)

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