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RISEffect of Trailing Edge and Span Morphing on the Performance of an Optimized NACA6409 Wing in Ground Effect
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A computational fluid dynamics (CFD) investigation was carried out on a three-dimensional NACA6409 wing in ground effect at a Reynolds number of 320,000. Using a multi-objective-SHERPA algorithm, a root angle of 4 deg angle ...