KSI ENGINEERING
PROPERTIES
OF AREAS
Toe Myint Naing
Curtin Malaysia
Intern
2Normal Stress Distribution
• When external axial loads are applied,
they are resisted by internal normal
stresses acting over the cross sectional
area of the section.
• When external bending moments are
applied, they need to be resisted by an
internal resisting couple. It therefore
follows that we need a first moment of area
to help determine the stresses in a beam
subjected to a moment.
(lbf/𝑖𝑛2)
(lbf/𝑖𝑛2)
©Curtin,CEM, Lec 2
3Properties of Areas
Need to have an understanding of Properties of Areas to be able to determine the stresses
due to bending
• Centre of Gravity,
Centroid (Neutral Axes)
• Second Moment of Area (I value)
• Elastic Section Modulus;
First Moment of Area (Z value)
The Centroid of a body is the point where
the entire weight of the body appears to be
concentrated.
Centroidal axis ≠ Equal area
axis
©Curtin,CEM, Lec 2
Centroid, Neutral Axis
General equation about the x-axis
4
©Curtin,CEM, Lec 2
Centroid, Neutral Axis
General equation about the y-axis
5
©Curtin,CEM, Lec 2
I-value, Second Moment of Area
I-value is a measure of the geometric stiffness of a shape
I-value allows us to quantify deflections and stresses depending upon the orientation of
the beam.
6
©Curtin,CEM, Lec 2
Ixx (second moment of area about the x-axis) in
order to quantify deflection and stresses when
bending about the x-axis.
Iyy (second moment of area about the y-axis) in
order to quantify deflection and stresses when
bending about the y-axis.
I-value, Second Moment of Area 7
©Curtin,CEM, Lec 2
𝐼(rectangle) =(
𝑏𝑑3
12
) + 𝐴ℎ2
=(
𝑏𝑑3
12
)
0
Equation for rectangular section
𝐼 = (
𝑏𝑑3
12
+ 𝐴ℎ2
)
I-value, Second Moment of Area 8
©Curtin,CEM, Lec 2
𝐼 = (
𝑏𝑑3
12
+ 𝐴ℎ2
)
General equation about the x-axis
Between centroid of whole section &
centroid of rectangle being considered
I-value, Second Moment of Area 9
©Curtin,CEM, Lec 2
General equation about the y-axis
Between centroid of whole section &
centroid of rectangle being considered
𝐼 = (
𝑏𝑑3
12
+ 𝐴ℎ2
)
I-value, Second Moment of Area 10
©Curtin,CEM, Lec 2
General equation about the x-axis
(Symmetric)
𝐼 = (
𝑏𝑑3
12
+ 𝐴ℎ2
)
I-value, Second Moment of Area 11
©Curtin,CEM, Lec 2
General equation about the y-axis
(Symmetric)
𝐼 = (
𝑏𝑑3
12
+ 𝐴ℎ2
)
First Moment of Area, Elastic Section Modulus (Z) 12
©Curtin,CEM, Lec 2
Equation for rectangular section
𝑍 𝑥 =
𝐼 𝑥
𝑦 𝑚𝑎𝑥
Normal Bending Stress 13
©Curtin,CEM, Lec 2
𝜎 𝑚𝑎𝑥 =
𝑀𝑦 𝑚𝑎𝑥
𝐼
𝑍 =
𝐼
𝑦 𝑚𝑎𝑥
∴ 𝜎 𝑚𝑎𝑥 =
𝑀
𝑍
∴ Stresses are related to the Z value
1
𝑅
=
𝑀
𝐸𝐼
∴ ∆=
𝑀
𝐸𝐼
(constant)
∴ Deflections are related to the I value
(and E)
Normal Bending Stress
Stresses when bending moments are applied about the x-axis
𝜎 𝑥 =
𝑀 𝑥 𝑦
𝐼 𝑥
𝑍𝑡𝑜𝑝 =
𝐼 𝑥
𝑦𝑡𝑜𝑝 𝑓𝑖𝑏𝑟𝑒
𝜎max 𝑡𝑜𝑝 =
𝑀 𝑥
𝑍𝑡𝑜𝑝
𝑍 𝑏𝑜𝑡 =
𝐼 𝑥
𝑦 𝑏𝑜𝑡 𝑓𝑖𝑏𝑟𝑒
𝜎max 𝑏𝑜𝑡 =
𝑀 𝑥
𝑍 𝑏𝑜𝑡
©Curtin,CEM, Lec 2
14
Normal Bending Stress
Stresses when bending moments are applied about the y-axis
𝜎 𝑦 =
𝑀 𝑦 𝑥
𝐼 𝑦
𝑍 𝐿𝐻𝑆 =
𝐼 𝑦
𝑦 𝐿𝐻𝑆 𝑓𝑖𝑏𝑟𝑒
𝜎max 𝐿𝐻𝑆 =
𝑀 𝑦
𝑍 𝐿𝐻𝑆
𝑍 𝑅𝐻𝑆 =
𝐼 𝑦
𝑦 𝑅𝐻𝑆 𝑓𝑖𝑏𝑟𝑒
𝜎max 𝑅𝐻𝑆 =
𝑀 𝑦
𝑍 𝑅𝐻𝑆
©Curtin,CEM, Lec 2
15
Thank
sFor your attention
Any
Question?

Properties of area presentation

  • 1.
    KSI ENGINEERING PROPERTIES OF AREAS ToeMyint Naing Curtin Malaysia Intern
  • 2.
    2Normal Stress Distribution •When external axial loads are applied, they are resisted by internal normal stresses acting over the cross sectional area of the section. • When external bending moments are applied, they need to be resisted by an internal resisting couple. It therefore follows that we need a first moment of area to help determine the stresses in a beam subjected to a moment. (lbf/𝑖𝑛2) (lbf/𝑖𝑛2) ©Curtin,CEM, Lec 2
  • 3.
    3Properties of Areas Needto have an understanding of Properties of Areas to be able to determine the stresses due to bending • Centre of Gravity, Centroid (Neutral Axes) • Second Moment of Area (I value) • Elastic Section Modulus; First Moment of Area (Z value) The Centroid of a body is the point where the entire weight of the body appears to be concentrated. Centroidal axis ≠ Equal area axis ©Curtin,CEM, Lec 2
  • 4.
    Centroid, Neutral Axis Generalequation about the x-axis 4 ©Curtin,CEM, Lec 2
  • 5.
    Centroid, Neutral Axis Generalequation about the y-axis 5 ©Curtin,CEM, Lec 2
  • 6.
    I-value, Second Momentof Area I-value is a measure of the geometric stiffness of a shape I-value allows us to quantify deflections and stresses depending upon the orientation of the beam. 6 ©Curtin,CEM, Lec 2 Ixx (second moment of area about the x-axis) in order to quantify deflection and stresses when bending about the x-axis. Iyy (second moment of area about the y-axis) in order to quantify deflection and stresses when bending about the y-axis.
  • 7.
    I-value, Second Momentof Area 7 ©Curtin,CEM, Lec 2 𝐼(rectangle) =( 𝑏𝑑3 12 ) + 𝐴ℎ2 =( 𝑏𝑑3 12 ) 0 Equation for rectangular section 𝐼 = ( 𝑏𝑑3 12 + 𝐴ℎ2 )
  • 8.
    I-value, Second Momentof Area 8 ©Curtin,CEM, Lec 2 𝐼 = ( 𝑏𝑑3 12 + 𝐴ℎ2 ) General equation about the x-axis Between centroid of whole section & centroid of rectangle being considered
  • 9.
    I-value, Second Momentof Area 9 ©Curtin,CEM, Lec 2 General equation about the y-axis Between centroid of whole section & centroid of rectangle being considered 𝐼 = ( 𝑏𝑑3 12 + 𝐴ℎ2 )
  • 10.
    I-value, Second Momentof Area 10 ©Curtin,CEM, Lec 2 General equation about the x-axis (Symmetric) 𝐼 = ( 𝑏𝑑3 12 + 𝐴ℎ2 )
  • 11.
    I-value, Second Momentof Area 11 ©Curtin,CEM, Lec 2 General equation about the y-axis (Symmetric) 𝐼 = ( 𝑏𝑑3 12 + 𝐴ℎ2 )
  • 12.
    First Moment ofArea, Elastic Section Modulus (Z) 12 ©Curtin,CEM, Lec 2 Equation for rectangular section 𝑍 𝑥 = 𝐼 𝑥 𝑦 𝑚𝑎𝑥
  • 13.
    Normal Bending Stress13 ©Curtin,CEM, Lec 2 𝜎 𝑚𝑎𝑥 = 𝑀𝑦 𝑚𝑎𝑥 𝐼 𝑍 = 𝐼 𝑦 𝑚𝑎𝑥 ∴ 𝜎 𝑚𝑎𝑥 = 𝑀 𝑍 ∴ Stresses are related to the Z value 1 𝑅 = 𝑀 𝐸𝐼 ∴ ∆= 𝑀 𝐸𝐼 (constant) ∴ Deflections are related to the I value (and E)
  • 14.
    Normal Bending Stress Stresseswhen bending moments are applied about the x-axis 𝜎 𝑥 = 𝑀 𝑥 𝑦 𝐼 𝑥 𝑍𝑡𝑜𝑝 = 𝐼 𝑥 𝑦𝑡𝑜𝑝 𝑓𝑖𝑏𝑟𝑒 𝜎max 𝑡𝑜𝑝 = 𝑀 𝑥 𝑍𝑡𝑜𝑝 𝑍 𝑏𝑜𝑡 = 𝐼 𝑥 𝑦 𝑏𝑜𝑡 𝑓𝑖𝑏𝑟𝑒 𝜎max 𝑏𝑜𝑡 = 𝑀 𝑥 𝑍 𝑏𝑜𝑡 ©Curtin,CEM, Lec 2 14
  • 15.
    Normal Bending Stress Stresseswhen bending moments are applied about the y-axis 𝜎 𝑦 = 𝑀 𝑦 𝑥 𝐼 𝑦 𝑍 𝐿𝐻𝑆 = 𝐼 𝑦 𝑦 𝐿𝐻𝑆 𝑓𝑖𝑏𝑟𝑒 𝜎max 𝐿𝐻𝑆 = 𝑀 𝑦 𝑍 𝐿𝐻𝑆 𝑍 𝑅𝐻𝑆 = 𝐼 𝑦 𝑦 𝑅𝐻𝑆 𝑓𝑖𝑏𝑟𝑒 𝜎max 𝑅𝐻𝑆 = 𝑀 𝑦 𝑍 𝑅𝐻𝑆 ©Curtin,CEM, Lec 2 15
  • 16.
  • 17.

Editor's Notes

  • #4 Unsystematical
  • #14 M= moment I= moment of inertia E= young's modulus R= radius of curvature y= distance of element from center axis 𝜎= stress