2020
DOI: 10.1007/s42452-020-2559-9
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Structural design of composite stiffened panel for a flat wing micro-aircraft

Abstract: In this study, the integral micro-sized composite wings are designed and manufactured by using carbon fiber reinforced plastics and low-density foam. The analytical expressions of bending stiffness of a multilayer sandwich structures for variable cross-section panel are determined. The obtained analytical bending stiffness is numerically verified using results of compressive buckling modes on wing panels from a numerical FE program and experimental tests by a series of stiffened structures which are empiricall… Show more

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