Laminates made with polyester or vinyl-ester resins can undergo substa
ntial shrinkage when subject to an elevated-temperature post-cure afte
r room-temperature polymerisation. In composite tubes, restraint on fr
ee shrinkage, which results in residual stresses, arises because the i
n-plane shrinkages tend to be substantially smaller than the through-t
hickness shrinkages and also because of differences in the shrinkages
of adjacent layers of different constructions. This paper presents the
results of a theoretical investigation of the associated residual str
esses. The Rayleigh-Ritz method is implemented in predicting the resid
ual stresses and results are presented for a range of cases representa
tive of practical materials, constructions and geometries. It is shown
that inner-wall tensile residual stresses of sufficient magnitude to
promote environmentally assisted cracking can readily be induced. Furt
hermore, the results indicate that the widely specified +/- 55 degrees
laminate construction tends to give rise to particularly unfavourable
residual stress states. (C) 1997 Elsevier Science Limited.