Zhaolin Chen1,*, Xiaohui Wei1, Tianhang Xiao1, Ning Qin2
The International Conference on Computational & Experimental Engineering and Sciences, Vol.25, No.2, pp. 1-1, 2023, DOI:10.32604/icces.2023.09976
Abstract A computational study has been conducted on various airfoils to simulate flows at low Reynolds numbers
17,000 and 21,000 with Mach number changes from 0.25 to 0.85 to provide understanding and guidance for
Mars rotory wing designs. The computational fluid dynamics tool used in this study is a Reynolds-averaged
Navier–Stokes solver with a transition model (k-ω SST γ-Reθ). The airfoils investigated in this study include
NACA airfoils (4, 5, and 6% camber), UltraThin airfoils, and thin cambered plates (3% camber, but various
maximum camber locations). Airfoils were examined for lift and drag performance as well… More >
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