Fatigue life prediction is investigated analytically for matrix dominated p
olymer composite laminates having nonlinear stress/strain response, based o
n the fatigue modulus concept. Fatigue modulus degradation rate at any fati
gue cycle was assumed as a power function of number of fatigue cycles. A ne
w stress function describing the relation of initial fatigue modulus and el
astic modulus was used to account for material non-linearity at the first c
ycle. It was assumed that fatigue modulus at failure is proportional to the
applied stress level. A new fatigue life prediction equation as a function
of applied stress is proposed. The prediction was verified experimentally
using cross-ply carbon/epoxy laminate (CFRP) tube under torsional fatigue l
oading. It is shown that the proposed equation has wide applicability and a
grees well with experimental data.