Mechanical Test B Flashcards
Loading Conditions of Mechanical tests (4)
- Monotonically Increasing (Static)
- High Strain Rate (i.e. Impact)
- Repeated (Fatigue)
- Sustained (Creep)
When and where do fatigue failures occur
Fatigue failures generally occur suddenly, without significant prior
deformation.
Most common in parts subjected to high cyclic loading:
Axles
Drive Shafts
Propeller Shafts & Blades
Crank Shafts
Can also occur in structural elements:
Aircraft wings & fuselage
Structures carrying high live loads (bridges)
Bracing, struts, ties
Two basic stages involved in fatigue failure:
- Crack initiation
- Crack propagation
Where do cracks typically initiate at a free surface at a point of high stress
concentration: (2)
Preexisting flaw
Discontinuity (thread root, hole, geometric change)
what are the two basic types of machines
Constant Load
Load cycle remains constant
Strain gradually increases as specimen sustains damage
Constant Displacement
Displacement cycle remains constant
Stresses change as specimen sustains damage
Drawbacks of Constant Moment Rotating Bending Machine
- Not suitable for nonzero mean
stress. - Specimen must be circular in
cross-section.
where does fatigue failure occur in concrete
paste aggregate interface
common types of fatigue loading
alternating- looks like a sin wave
partly reversed- sin wave moved up a little
pulsating- sin wave with base of wave just touching the x axis
pulsating- all above x axis
random
what causes random fatigue loadings
seismic
wind
waves
Variability in Fatigue Testing Results:
- For real materials, containing imperfections of various kinds, no two samples are truly identical.
- It is virtually impossible to reproduce precisely the same test conditions over a large number of tests.
problems with the palmgren-miner hypothesis (linear damage rule)
- assumes that the damage accumulating in each cycle of loading is independent of stress history - not true
- assumes that there is no effect due to the order in which direct stress levels are applied - not true
Stress concentration severity increases with:
- increasing flaw size
- decreasing radius of curvature of flaw tip
material properties and fatigue
Grain Size:
Finer grain size improves fatigue resistance.
Surface Finish:
Smooth surfaces less susceptible to crack initiation.
Surface Finish:
Grinding, plating, milling etc. all affect crack initiation potential.
Residual Stresses in Surface:
Tensile - reduce fatigue life
Compressive - improve fatigue life
environmental conditions and fatigue
increase temp decreases fatigue life
fatigue limits may disappear at high temperatures
thermal cycling can induce stresses that lead to thermal fatigue if the material is restrained from expanding/contracting.
corrosion
Surface pitting provides crack initiation points.
Fatigue limits disappear in corrosive environments.