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Tag Archives: computational

EFFECT OF ANGLE OF ATTACK, GAS COMPOSITION AND REYNOLDS NUMBER ON FLUTTER BOUNDARY OF BENCHMARK SUPER-CRITICAL WING

1.Events, Computational Aeroelasticity, IFASD 2017By Beata Wierzbińska-PrusAugust 21, 2024

Jan Navrátil, Adam Jirásek, Peter Hamlington, Lt. Col. Andrew Lofthouse

DOI Number: N/A

Conference number: IFASD-2017-142

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