Abstract
As stated in Sect. 4.9, the axisymmetry of the load for a circular cylindrical shell means that the axial load component \( p_{x} \) and normal load component \( p_{z} \) are uniformly distributed along the circumference, and the circumferential load component \( p_{\uptheta } \) is zero. This chapter deals with the analysis of circular cylindrical shells with edges for \( x = {\text{constant}} \) under axisymmetric loading. We put \( p_{x} \) to zero, so consider only a normal load \( p_{z} \).
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Reference
Bouma AL et al (1958) Edge disturbances in axi-symmetrically loaded shells of rotation. IBC announcements, Institute TNO for Building Materials and Building Structures, Delft (in Dutch)
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© 2014 Springer Science+Business Media Dordrecht
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Blaauwendraad, J., Hoefakker, J.H. (2014). Edge Disturbance in Circular Cylindrical Shells Under Axisymmetric Load. In: Structural Shell Analysis. Solid Mechanics and Its Applications, vol 200. Springer, Dordrecht. https://doi.org/10.1007/978-94-007-6701-0_5
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DOI: https://doi.org/10.1007/978-94-007-6701-0_5
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