In the previous chapter, Euler-Bernoulli theory is developed for beams under axial and transverse loads. The analysis is limited, however, to deformations of the beam in plane (ī1, ī2). This behavior can be observed, for instance, when the cross-section of the beam presents a plane of symmetry and the only applied loads are acting in this plane.
In numerous practical applications, the beam's cross-section presents no particular symmetries and is instead of arbitrary shape. In addition, the applied loads may act along several distinct directions and not just in plane (ī1, ī2). Consider an aircraft wing: the cross-section is of a complex shape involving curved skins and two or more spars, and the wing is subjected lift and drag forces. In the case of a helicopter blade, large centrifugal forces generated by the rotation of the blade are also present. Similarly, machine components often operate in a complex, three-dimensional loading environment.
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Bauchau, O.A., Craig, J.I. (2009). Three-dimensional beam theory. In: Bauchau, O.A., Craig, J.I. (eds) Structural Analysis. Solid Mechanics and Its Applications, vol 163. Springer, Dordrecht. https://doi.org/10.1007/978-90-481-2516-6_6
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DOI: https://doi.org/10.1007/978-90-481-2516-6_6
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