Generic Approach to Determine Optimum Aeroelastic Characteristics for Composite Forward-Swept-Wing Aircraft

DOI10.2514/3.48423zbMath0533.73048OpenAlexW2041036682MaRDI QIDQ3316712

Gabriel A. Oyibo

Publication date: 1984

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.48423

zbMATH Keywords

transformationaeroelastic tailoringaeroelastic equations of motionall variables have to be consideredcomposite swept wingcritical aeroelastic characteristics for flutter and divergenceexpressible in terms of three bounded generic stiffness variables and the fiber orientation anglemultivariable optimization problem

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Composite and mixture properties (74E30) Optimization problems in solid mechanics (74P99) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

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