Visualizing three-dimensional effects of synthetic jet flow control
Author:
Funder
Natural Sciences and Engineering Research Council of Canada
Digital Research Alliance of Canada
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s12650-024-00992-0.pdf
Reference23 articles.
1. Amitay M, Glezer A (2002) Role of actuation frequency in controlled flow reattachment over a stalled airfoil. AIAA J 40(2):209–216. https://doi.org/10.2514/2.1662. (ISSN 0001-1452)
2. Amitay M, Smith DR, Kibens V, Parekh DE, Glezer A (2001) Aerodynamic flow control over an unconventional airfoil using synthetic jet actuators. AIAA J 39(3):361–370. https://doi.org/10.2514/2.1323. (ISSN 0001-1452)
3. Andino MY, Lin JC, Washburn AE, Whalen EA, Graff EC, Wygnanski IJ (2015) Flow separation control on a full-scale vertical tail model using sweeping jet actuators. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2015-0785. (ISBN 978-1-62410-343-8)
4. Balzer W, Fasel H (2010) Direct numerical simulation of laminar boundary-layer separation and separation control on the suction side of an airfoil at low reynolds number conditions. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-4866. (ISBN 978-1-60086-956-3)
5. Batill SM, Mueller TJ (1981) Visualization of transition in the flow over an airfoil using the smoke-wire technique. AIAA J 19(3):340–345. https://doi.org/10.2514/3.50953. (ISSN 0001-1452)
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