Reynolds Number and Freestream Shear Effects on a NACA 0012 Airfoil in the Reynolds Number Range 10,000-30,000
1980 ◽
Vol 101
(4)
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pp. 721-735
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2019 ◽
Vol 77
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pp. 113-121
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2014 ◽
Keyword(s):
2006 ◽
Vol 110
(1105)
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pp. 145-156
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2015 ◽
Vol 95
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pp. 22-33
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