Aerodynamic study of a circular arc airfoil at low Reynolds numbers using Cartesian mesh CFD
Author:
Affiliation:
1. Graduate School of Environmental Science, Hokkaido University
2. Department of Aeronautics, Kanazawa Institute of Technology
Publisher
Japan Society of Mechanical Engineers
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering
Link
https://www.jstage.jst.go.jp/article/jfst/17/3/17_2022jfst0007/_pdf
Reference14 articles.
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2. Dutta, S., Karlgaard, C. D., Kass, D., Villar, G. and Mischna, M., Post-flight Analysis of Atmospheric Properties from Mars 2020 Entry, Descent, and Landing, AIAA SCITECH 2022 Forum (2022), AIAA Paper 2022-0422.
3. Luong, R., Nagai, H. and Asai, K., Conceptual Design of Mars Airplane, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol.10, Issue ists28 (2012), pp.Te_5–Te_10.
4. Iioka, D., Fukuda, K., Okamoto, M., Sasaki, D., Shimoyama K. and Obayashi S., Computational Analysis of Thin Airfoils under Low Reynolds Number Flow Using Block-Structured Cartesian Mesh, 55th AIAA Aerospace Sciences Meeting (2017), AIAA Paper 2017-0546.
5. Lee, D., Kawai, S., Nonomura, T., Anyoji, M., Aono, H., Oyama, A., Asai, K. and Fujii, K., Mechanisms of Surface Pressure Distribution within a Laminar Separation Bubble at Different Reynolds Numbers, Physics of Fluids, Vol.27, Issue 2, 023602 (2015).
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