Open AccessDesign of cylindrical composite panels with mild camber for biaxial compression taking into account geometrical non-linearity with uniform heating and rigid support
Author(s) -
O. V. Mitrofanov,
M. V. Klesareva
Publication year - 2019
Publication title -
iop conference series. materials science and engineering
Language(s) - English
Resource type - Journals
eISSN - 1757-899X
pISSN - 1757-8981
DOI - 10.1088/1757-899x/684/1/012019
Subject(s) - camber (aerodynamics) , buckling , structural engineering , composite number , materials science , boundary value problem , compression (physics) , composite material , engineering , mathematics , mathematical analysis
Based on geometrically non-linear task analytic solution for cylindrical composite panel with mild camber method of best possible design for post-buckling state with biaxial compression is suggested. Uniform heating and panel all-boundary rigid support are taken into account in basic correlations.