GEOMETRICALLY NONLINEAR MODEL FOR GUST RESPONSE OF VERY FLEXIBLE WINGS USING SEGMENTAL MODES

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Veröffentlicht in:AIAA SciTech Forum and Exposition (2021 : Online) Structural dynamics ; Volume 2 of 2
1. Verfasser: Gov, Favel (VerfasserIn)
Weitere Verfasser: Karpel, Moti (VerfasserIn)
Pages:2
Format: UnknownFormat
Sprache:eng
Veröffentlicht: 2021
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