Pressure Improvement on a Supercritical High-Lift Wing Using Simple and Modulated Pulse Jet Vortex Generator
Author:
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/s10494-022-00327-9.pdf
Reference63 articles.
1. Abdolahipour, S., Mani, M., Taleghani, A.S.: Parametric study of a frequency-modulated pulse jet by measurements of flow characteristics. Phys. Scr. 96(12), 12–5012 (2021)
2. Abdolahipour, S., Mani, M., Taleghani, A.S.: Enhancing the high-lift properties of a supercritical wing by means of a modulated pulse jet actuator. Tech. Phys. Lett. (2022). https://doi.org/10.21883/PJTF.2022.01.51869.18999
3. Aley, K., Guha, T.K., Kumar, R.: Experimental characterization of a high-lift supercritical airfoil with microjets. In: 2018 flow control conference (p. 3688) (2018).
4. Aley, K., Guha, T.K., Kumar, R.: Active flow control of a high-lift supercritical airfoil with microjet actuators. AIAA J. 58(5), 2053–2069 (2020)
5. Amitay, M., Glezer, A.: Role of actuation frequency in controlled flow reattachment over a stalled airfoil. AIAA J. 40(2), 209–216 (2002a)
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