The paper deals with fatigue crack propagation from notches in plates made of FeP04 steel and AA 356-T6 aluminium alloy. The tests were performed under different stress ranges by keeping constant the nominal load ratio (R=0.1). The specimens were weakened by nearly-sharp and blunt two-sided notches. The results of the fatigue tests are reanalysed here in terms of J-integral range including the notch influence. It was observed that the blunter notches are, the higher fatigue crack growth rate is.
JavaScript jest wyłączony w Twojej przeglądarce internetowej. Włącz go, a następnie odśwież stronę, aby móc w pełni z niej korzystać.