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Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
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Design, development and approbation of the numerical technique in simulating the wing aeroelastic state based on the finite element and control volumes methods

Published: 20.07.2023

Authors: Gunchin V.K., Bolshikh A.A., Ustinov B.E.

Published in issue: #7(139)/2023

DOI: 10.18698/2308-6033-2023-7-2291

Category: Aviation and Rocket-Space Engineering | Chapter: Design, Construction, Production, Testing, and Operation of Aircraft

    aerodynamics, strength, finite element model, aeroelasticity, aerodynamic loads
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