NASA NTRS · 19750000094
Computer program for numerical analysis of stiffened shells of revolution
Abstract
Programs, using Love-Reissner first-order shell theory, can analyze orthotropic thin shells of revolution subjected to unsymmetric distributed loading or concentrated line loads and thermal strains. They can perform stability or vibration analysis of thin shells of revolution subjected to axisymmetric distributed loading or concentrated line loads and thermal strains.
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Key, J., Svalbonas, V.. 1975-06-01. Computer program for numerical analysis of stiffened shells of revolution. https://ntrs.nasa.gov/citations/19750000094
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