C6 Failure Flashcards
type of failure
2 types
- ductile
- brittle
elobrate
ductile
- occur at high temp
- show plastic deform
- has 5 cup-cone fracture stage
elobrate
brittle
- occur at low temp
- not showing any deform
- break without warning
- when look at microscope can see thin line sample fail
what are
stages in cup-and-cone fracture
- necking
- cavity formation
- coalescence cavities form crack
- crack propagation
- fracture
the sharp tip in sample crack can causing
it propogate crack
how to stop crack growth
blunt the tip
crack growth condition
K ≥ Kc = Yθ√(πa)
Y=material behaviour, a=area
Formula for: θ (y-axis) vs a max (x-axis)
θ design < Kc / Y(√πa max)
Formula for graph: a max (y-axis) vs θ (x-axis)
a max < (1/π) [Kc / Y(θ design)]^2
for both graph: (a max vs θ) & (θ vs a max)
the area under graph means
no fracture
for both graph: (a max vs θ) &
the area above graph means
fracture
ductile brittle transition test
charpy experiment test
charpy experiment test conduct at diff temp
- to the left (low temp): brittle
- to the right (high temp): ductile
- impact energy = (max - min) / 2
Type application of failure
- Fatigue
- Creep
what is fatigue
- predict max cycle
- repeated cycling load
what is creep
- predict max time
- time dependent deform due to constant load at high temp
low cycle fatigue
small no of cycle
* high load
* plastic & elastic deform
high cycle fatigue
large no of cycle
* low load
* elastic deform (N>10^5)
type of fatigue behaviour :
fatigue limit Sfat : no fatigue is S < Sfat
Fatigue S-N curves
above graph: unsafe
below graph: safe
type of stress for fatigue test
3 types
- axial (tension-compression)
- flexural (bending)
- torsional (twisting)
mean stress, σm
(σmax + σmin) / 2
stress amplitude, σa
(σmax - σmin) / 2
stress range, σr
σmax - σmin
stress ratio, R
σmin / σmax
Factors affect fatigue life
- magnitude of stress
- quality of stress
what is solution
- polish surface
- introduce compressive stress into surface area
- case hardening
- optimize geometry
- avoid internal corners
environmental effect
thermal fatigue solution
- change design
- use material with low thermal expansion coefficient
environmental effect
corrosion fatigue solution
- decrease corrosiveness of medium
- add protective surface coating
- add residual compressive stress
improve fatigue life
- impose a compressive surface stress ( to suppress surface crack growth
- remove stress concentrators
2 method : shot peening & caburizing
prediction of creep rupture lifetime
T(20 + log tr) = L
T= temp,K . tr= time rupture/failure . L= function of applied stress
materials that resilent to creep
resilient = tahan
- stainless steel
- refractory metals (contain element high m.p. eg;Nb, Ta)
- superalloys (Co, Ni based)