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Tag Archives: UVLM (unsteady vortex lattice method)

GUST RESPONSE ANALYSIS FOR HIGH-ASPECT RATIO WING

2. IFASD 2015, Aeroelastic Response & StabilityBy Beata Wierzbińska-PrusNovember 19, 2024

Liu Yi, Xie Changchuan, Yang Chao

DOI Number: N/A

Conference number: IFASD-2015-126

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