An elastic-plastic stress analysis has been carried out in a stainless stee
l fiber reinforced aluminum matrix composite beam. The beam is loaded by a
single force at its free end. The composite material is assumed perfectly p
lastic to simplify the investigation. An exact solution is given for the el
astic and elastic-plastic regions. Orientation angles of the fiber are chos
en as 0 degrees, 30 degrees, 45 degrees, 60 degrees and 90 degrees. The pla
stic zone expands at the upper side of the beam more than at the lower side
for 30 degrees, 45 degrees and 60 degrees orientation angles. Residual str
ess components of sigma (x) and tau (xy) are found in the sections of the b
eam. The plastic collapse occurs at the different points for the beam of 0
degrees, 30 degrees, 45 degrees, 60 degrees and 90 degrees orientation angl
es.