NASA NTRS · 19700048444
Minimum weight design of stiffened cylinders
Abstract
Minimum weight design for symmetrically stiffened cylindrical shells under compression based on linear orthotropic stability theory
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Gerard, G., Lakshmikantham, C.. 1970-02-01. Minimum weight design of stiffened cylinders. https://ntrs.nasa.gov/citations/19700048444
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