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This document presents an experimental study on the leading edge vortices (LEVs) and stall behavior of nonslender delta wings, specifically focusing on wings with 50° and 65° leading edge sweeps. Conducted in a water tunnel, the research utilized stereoscopic digital particle image velocimetry to analyze the flow characteristics at various angles of attack, revealing significant differences in LEV behavior and stall onset between the two wing configurations. The findings suggest that the 50° wing experience

Author

Vivek Diwakar

Language

EN