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Minimum-mass optimization of composite stiffened, unstiffened and sandwich curved panels subjected to combined longitudinal and transverse compression and shear loading
No full textBuckling Load of Several Types (Sandwich, Blade, T and Hat-stiffened) Cylindrical Composite Panels Subjected to Biaxial Compression and Shear Load as Typical Application to an Aircraft Fuselage (Theoretical Analysis and User's Manual of the Optimization Computer Program OPTICO) (Calcolo del carico di buckling per diversi tipi di soluzione (nido d'ape, irrigidimento ad I, T, Omega) e di vincolo di pannelli a semplice curvatura in materiale composito soggetti a carico combinato di sforzi normali e taglio con applicazione ad una fusoliera di velivolo militare (Analisi teorica finale e manuale di impiego del programma di ottimizzazione OPTICO)
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"Minimum-mass optimization of composite stiffened, unstiffened and sandwich curved panels subjected to combined longitudinal and transverse compression and shear loading".
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Early warning Systems (EWSs) and Business Crisis: Building and Updated Co-operative Multidisciplinary Institutional Approach for Tax Agencies
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