Transonic Static Aeroelastic Numerical Analysis of Flexible Complex Configuration Wing
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DOI: 10.1155/2021/5553304
Abstract: Diamond back wing is subjected to large deformation while gliding, which significantly changes characteristics of the lift as well as the static stability. For this reason, conventional rigid aircraft assumption cannot meet the requirements of… read more here.
Keywords: transonic static; numerical analysis; analysis; analysis flexible ... See more keywords