In this study a method has been developed for the calculation of effec
tive moduli of filament wound composite tubes. Composite tubes made of
two different types of fibres and an epoxy resin are tested for tensi
on and inner pressure for three different patterns and three different
winding angles. Using the results of pressure test and the properties
obtained from coupon tests, and applying laminated composite plate th
eory, the elastic moduli are determined. Calculated elastic moduli are
then checked by using the data obtained from the tension tests. Resul
ts for effective moduli are tabulated for different winding patterns a
nd different winding angles.