In order to obtain stress ratio as well as stress intensity factor range wh
ich was applied on the material before failure from the fracture surface ob
servation, the effect of stress ratio on fatigue striation height has been
investigated on two different alloys (an Fe-3% Si single crystalline alloy
and a 7075 polycrystalline aluminium alloy). Striation height has been meas
ured both microscopically using a scanning tunnelling microscope and macros
copically using a scanning electron microscope. Striation height increased
with decreasing stress ratio on both the materials at a given crack growth
rate. This tendency was found by all the measuring methods used. This sugge
sts that not only stress amplitude but also stress ratio which were applied
on the material before the failure could be obtained by post-failure analy
sis. (C) 1999 Kluwer Academic Publishers.