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The effect of plain and trailing edge Gurney flaps on a non-slender delta wing is characterized experimentally and simulated analytically. The results show that plain trailing edge flaps are more efficient than Gurney flaps.
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This page is a summary of: Effects of Plain and Gurney Flaps on a Nonslender Delta Wing, Journal of Aircraft, October 2018, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c034929.
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