The role of mechanical properties of composite material in dome contou
r design has been investigated. It has been shown that the optimal dom
e profile depends on the ratio of longitudinal Young's modulus to tran
sverse Young's modulus in individual laminae (E(x)/E(y)). This profile
for any type of composite material always lies between the Netting An
alysis solution (E(y) = 0, E(x)/E(y) = infinity) and a semi-circle whi
ch is the solution for the square symmetric (E(x)/E(y) = 1) and isotro
pic materials. The shells of revolution of double curvature, classical
lamination theory (CLT) and the geodesic-isotensoid assumptions have
been used.