Environmental Engineering Reference
In-Depth Information
Fig. 4.38 Failure curves for the biaxial stress state S
cd,min
¼0.6
Fig. 4.39 Failure curves for the biaxial stress state S
cd,min
¼0.8
with higher numbers of fatigue cycles is greater for biaxial repeated compressive loads
(
s
11
¼s
22
) than for uniaxial ones. This can be attributed to the different courses of the
damage variables in the high-cycle range. It is obvious that up to approx. log N
¼
8, the
biaxial fatigue strength for repeated compressive loads is greater than the uniaxial
fatigue strength. This no longer applies when log N
¼
10. The failure curve for