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Analysis of Bi-stable Hexagonal Composite Laminate Under Thermal Load
Veröffentlicht in Applied composite materials
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Nonlinear aeroelastic response of slender wings based on Wagner function
Veröffentlicht in Thin-walled structures
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An efficient method for nonlinear aeroelasticy of slender wings
Veröffentlicht in Nonlinear dynamics
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Free-edge effects analysis of angle-ply laminates under transverse loading using layer-wise finite-element method with semi-analytical shear stress calculation
Veröffentlicht in Proceedings of the Institution of Mechanical Engineers. Part C, Journal of mechanical engineering science
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