BMEE209L: Module 4 (UPDATED) Flashcards
(32 cards)
Define stress
Force per unit area
Define strain
How much deformation has occurred with that applied force
Elastic Deformation
The linear part of the stress strain curve; at this stage when the force is removed the material will revert back to its original shape
Yield Strength
A point on the stress-strain curve above which any additional stress will cause permanent deformation
What happens when the materials reaches Ultimate Strength point in the stress-strain curve?
After that point, less stress is needed as the material begins to decrease its cross-section, through a process called necking, which continues until the material fractures
Poisson’s Ratio
- (Lateral Strain/Longitudinal Strain)
Modulus of Resilience
1/2 x yield strength x strain at yielding
Tensile Toughness
Energy absorbed by a material prior to fracturing
Ductility
Amount of deformation a material can withstand without breaking
Tensile Strength/Ultimate Strength
UTS = Fmax/A0
How to determine 0.2% offset yield strength
when a yield point isn’t sharply defined:
1) Start at strain = 0.002
2) Draw a line parallel to linear region of curve
3) Point of intersection is the yield strength
Modulus of elasticity
Young’s Modulus = stress/strain
True stress strain curve vs Engineering stress strain curve
True stress strain curve will always keep increasing while the engineering stress strain curve will drop during necking
True stress
σt = σe(1+εe)
True strain
εt = ln(1+εe)
Effect of temperature on stress strain curve
High temperature: curve shifts downwards and more to right becomes soft and ductile
Low temperature: curve shifts up and more to left
becomes hard and brittle
Brinell Hardness
BHN = 2P/piD(D-sqrt(D^2-d^2))
where P = load
D = diameter of ball indenter
d = diameter of indentation
Rockwell Hardness
N - h/S
N = scale factor
h = depth of indentation
S = scale division factor
Lower strain rate means material is
ductile
Higher strain rate means material is
brittle
Among BCC and FCC metals which have ductile to brittle transition temperatures
BCC (iron, tungsten) metals do but FCC(aluminium, copper) metals do not
Fracture toughness
K = fσsqrt(pia)
Fatigue
Lowering of strength or failure of a material due to repetitive stress which may be above or below the yield strength
Stages of Fatigue
1) Crack formation
2) Crack Growth
3) Fracture