15 research outputs found

    Flap-Torsion Coupling in Prismatic-Sections

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    Some Basic Strategies for Aeroelastic Tailoring of Wings with Bend-Twist Coupling: Part One

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    Composite Box Beam Analysis: Theory and Experiments

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    This paper presents two comprehensive analysis methodologies for composite beams and describes experimental results obtained from a thin-walled, rectangular cross-sectional beam. The theoretical predictions are found in good agreement with the observed twist and strain distributions. Out-of-plane torsional wraping of the cross-section is found to be the key factor for an accurate modeling of the torsional behavior of such structures. The upper and lower panels of the beam are graphite/epoxy laminated plates with aluminum C-channels forming the webs

    Response of a Three-Layered Ring to an Axisymmetric Impulse

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