fracture mechanics in fatigue analysis
DESCRIPTION
Fracture Mechanics in Fatigue Analysis. Mods for Factor “K”. The stress intensity factor K: a : the crack width and geometrical correction factor. - PowerPoint PPT PresentationTRANSCRIPT
Fracture Mechanics in Fatigue Analysis
The stress intensity factor K:
a: the crack width and geometrical correction factor.
F: the product of a couple of factors (back crack shape factors, front face factor, finite thickness factor, finite width factor and stress gradient factor)
K a F Mods for Factor “K”
Kmax and Kmin are the maximum and minimum values of the stress intensity factor, at theupper and lower limit stresses during a cyclic loading.
Kmax= F.σmax(π.a)1/2
Kmin= F.σmin(π.a)1/2
Plastic Zone Size =
∆σ1=(σ1max-σ1min)
Semi-Crack Lenght- Number of Cycles
∆K= Kmax-Kmin=F.∆σ(πa)1/2
Plastic Zone Characterized with K
Three distinct regions are indicated: 1) the well-known threshold region2) intermediate region3) the failure region.
max min
( )mda
C KdNK K K
m: experimental constantm= 3 for steelm=3~4 for aluminum alloy
Paris Law
Paris Law in Application
Differences Between Classical Design and
Fracture Mechanics Based Design
•Classical desing predicts that the material under pressure is confident under yield criteria.
•Classical desing ignores behaviours of material. (Ductile or Brittle)
•Classical design does not consider crack in the material and the fracture roughness
Infamous Fatigue Failures
War ship: S.S. Schenectady
Infamous Fatigue Failures
Offshore platform: Alexander Kielland
Infamous Fatigue Failures
Aircraft : De Havilland Comet