Abstract
… inverted airfoil in ground effect is investigated experimentally. The airfoil used is CLARK-Y … an incompressible airfoil chord length Reynolds numbers of 4.96×105, 5.96×105, 6.95×105 …
Cite
CITATION STYLE
APA
Y., I., & S., M. (2016). Experimental Study of CLARK-Y Smoothed Inverted Wing with Ground Effect. International Journal of Computer Applications, 147(1), 45–54. https://doi.org/10.5120/ijca2016910962
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