engineering materials lec 05
TRANSCRIPT
-
7/29/2019 Engineering Materials Lec 05
1/29
Haseeb Ullah Khan JatoiDepartment of Chemical Engineering
UET Lahore
-
7/29/2019 Engineering Materials Lec 05
2/29
-
7/29/2019 Engineering Materials Lec 05
3/29
Non-Destructive Testing (NDT) Using Physical Material Properties
Radiography (Radiations); Dye Penetrant (Color);
Ultrasonic (Ultrasounds); Magnetic Particle forcracks (Magnetic)
Destructive Testing (DT) Utilizing mechanical properties Push, Pull, Indent, Twist etc involved
-
7/29/2019 Engineering Materials Lec 05
4/29
A material with the highest electrical
conductivity in the world is of little utility if
its mechanical properties are not adequate
to allow it to be formed into wire, bent
round a switch lug, and held with a screw
-
7/29/2019 Engineering Materials Lec 05
5/29
-
7/29/2019 Engineering Materials Lec 05
6/29
Specimens are pulled, bent, twisted, compressed and sheared until
they break
-
7/29/2019 Engineering Materials Lec 05
7/29
Strain is the change in length occurring inmaterial with applied stress
In the beginning, material reverts back to
original shape when stress is lower(Elasticity)
As test proceeds, stress increases, andlength within gage region becomes longer
Stress-strain curve is linear hitherto, andslope is called Elastic Modulus
-
7/29/2019 Engineering Materials Lec 05
8/29
Material exhibiting linear stress-strain curve inthe elastic range are Hookean (after RobertHooke)
Modulus of Elasticity = E =stress/ strain
Over a range of stresses this curve begins todeviate from linearity
This transition from linearity occurs at a pointcalled proportional limit
Material may exhibit non-linear elastic behaviorabove proportional limit (Non-Hookean)
-
7/29/2019 Engineering Materials Lec 05
9/29
Further stress applied takes material toward
plastic deformation
Releasing the stress at this point makes the
material to be elongated from original length,called Plastic deformation
This point of transition from elastic to plastic
is termed Elastic limit, or Yield pointMeasured at an offset strain of 0.2% as this
point is difficult to measure
-
7/29/2019 Engineering Materials Lec 05
10/29
Further stress decreases the cross sectionalarea as length elongates
Material continues to harden and getsstronger, at the same time reducing crosssectional area, reducing the load-carryingcapacity
Force curve reaches a peak, called ultimatetensile strength
At this point, reduction in cross sectional areaoccurs in a pronounced localized spot, calledNecking
Ultimately, sample fractures into two halves
-
7/29/2019 Engineering Materials Lec 05
11/29
-
7/29/2019 Engineering Materials Lec 05
12/29
-
7/29/2019 Engineering Materials Lec 05
13/29
-
7/29/2019 Engineering Materials Lec 05
14/29
-
7/29/2019 Engineering Materials Lec 05
15/29
Two measurements made:
Final length of gage area is measured
Final diameter of the necked-down portion ofsample is measured
-
7/29/2019 Engineering Materials Lec 05
16/29
A measure of materials ability to bestretched or drawn
It is typically reported as percent
elongation or percent reduction in area
Percent Elongation =More this % elongation, more the ductilitySimilarly,
% reduction in area =
gthInitialLen
gthInitialLenhFinalLengt
aInitialAre
FinalAreaaInitialAre
-
7/29/2019 Engineering Materials Lec 05
17/29
Engineering Stress-strain curve: The stress values in engineering stress-strain curves
are calculated by dividing the force measured duringtensile test by original cross sectional area of
specimen. Similarly, strain is also calculated fororiginal length
True Stress-strain curve: The stress is calculated by dividing the force
measured during the tensile test by actual orinstantaneous cross-sectional area of the specimen.Similarly, strain is calculated with instantaneous gagelength
-
7/29/2019 Engineering Materials Lec 05
18/29
true = Kntrue
-
7/29/2019 Engineering Materials Lec 05
19/29
When material is plastically deformed,
interactions with dislocations in materials
structure can cause the material to become
stronger and harder. This phenomenon isWork hardening, or Strain hardening true = K
ntrue (True curve on graph)
true
= true stress
true = true strain
K = strength coefficient
n = strain hardening exponent
-
7/29/2019 Engineering Materials Lec 05
20/29
-
7/29/2019 Engineering Materials Lec 05
21/29
-
7/29/2019 Engineering Materials Lec 05
22/29
Modulus of elasticity
Yield strength
Ultimate tensile strength
Ultimate strength/yield strength (work
hardening)
Percent elongation
Percent reduction in areaGeneral shape of curve to evaluate
properties
-
7/29/2019 Engineering Materials Lec 05
23/29
Resilience is the property that defines a
materials ability to absorb elastic energy
Area under the elastic portion of stress-
strain curve provides an indication of
materials resilience
-
7/29/2019 Engineering Materials Lec 05
24/29
-
7/29/2019 Engineering Materials Lec 05
25/29
The ability of the material to absorb energy
before fracturing
Total area under the stress-strain curve up
to the point of fracture is toughness of the
material
-
7/29/2019 Engineering Materials Lec 05
26/29
-
7/29/2019 Engineering Materials Lec 05
27/29
-
7/29/2019 Engineering Materials Lec 05
28/29
Shear stress measured in tensile tester usingspecial grips
Shear yield strength 57.7% of tensile yield
strength (Mises-Henskey distortion energy theory for ductile materialfailure)s = Gs
s = shear stress,s = shear strain, G = shear modulus
The shear modulus is an importantproperty for calculating the stiffness orrigidity
-
7/29/2019 Engineering Materials Lec 05
29/29
Applying stress-strain relation in chemical
engineering design (Examples)
Iron and steel