Long-term two-dimensional analysis of the flow field around a hovering flapping flat-plate wing
Author:
Affiliation:
1. Institute of Fluid Science, Tohoku University
2. Department of Materials Science and Engineering, University of Washington
Publisher
Japan Society of Mechanical Engineers
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering
Link
https://www.jstage.jst.go.jp/article/jfst/18/2/18_2023jfst0026/_pdf
Reference38 articles.
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3. Aono, H., Kikkawa, K., Ishikawa, H. and Kang, C.-K., ’A numerical study of sound generation on pitch and plunge wing at low reynolds numbers’, in AIAA Scitech 2020 Forum (2020), p. 1495.
4. Bayiz, Y., Ghanaatpishe, M., Fathy, H. and Cheng, B., Hovering efficiency comparison of rotary and flapping flight for rigid rectangular wings via dimensionless multi-objective optimization, Bioinspiration & biomimetics, Vol. 13, No. 4 (2018), p. 046002.
5. Benedict, M., Coleman, D., Mayo, D. B. and Chopra, I., Experiments on rigid wing undergoing hover-capable flapping kinematics at micro-air-vehicle-scale reynolds numbers, AIAA Journal, Vol. 54, No. 4 (2016) pp. 1145–1157.
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