Skip to main content

Poisson’s ratio

 Poisson’s ratio 

It is the ratio of lateral strain to longitudinal strain and it is constant with in the elastic limit of the material. 
Poisson's Ratio is generally denoted by 'μ ' or u

The ratio is named after the French mathematician and physicist Siméon Poisson.
Note:
The tensile longitudinal stress produces compressive lateral strains or the compressive longitudinal stress produces tensile lateral strains.
(+ve Longitudinal strains produce -ve lateral strains or vice versa)  
 
Let us consider a rectangular bar of cross section (bxd) and length l and it is subjected to a axial load acts in the direction of length of the bar.
The longitudinal tensile strain in the bar 
longitudinal = δl / l
Lateral compressive strains in the directions of breadth b and  depth d of bar
elateral = δb/ b and 
elateral  =  δd /d
where δl = Change in length
δb = Change in width =b' - b
δd = Change in depth = d' - d
The poisson's Ratio
 
                      m = elateral / longitudinal
Lateral strain ,elateral = m.elongitudinal
Note:
Perfectly incompressible isotropic material deformed elastically at small strains would have a Poisson's ratio of exactly 0.5.
Example: Rubber has a Poisson ratio of nearly 0.5. and Cork's Poisson ratio is close to zero. Most of the metals it is in between 0.25 to 0.33

Examples:

1.A metal rod 20 mm diameter and 2 m long is subjected to a tensile force of 60 kN, it showed and elongation of 2 mm and reduction of diameter by 0.006 mm. Calculate the Poisson's ratio.
Solution:
The longitudinal strain = longitudinal = δl / l
                                    =  2mm/ 2000 = 0.001
The Lateral Strain = elateral   δd /d
                              = 0.006mm/20mm =0.0003
The poisson's Ratio = m = elateral / longitudinal
                                                = 0.0003/0.001 = 0.3 Ans.

Assignment :
1. A metal bar 50mmx50mm in section is subjected to an axial compressive load of 500 kN. If the contraction of a 200mm gauge length was found to be 0.5 mm and the increase in thickness 0.04 mm, find Poisson’s ratio.
(Ans: Poisson's ratio=0.32)
2.A steel rod 4 m long and 20mm diameter is subjected to an axial tensile load of 45 kN. Find the change in length and diameter of the rod. If
E= 200 GPa, and = 0.25
(Ans: Change in length=2.86mm, change in diameter =0.003575mm)
3. A steel rod 3m long and 25mm diameter is subjected to an axial tensile load of 60 kN. Calculate the change in length and diameter of rod. Take E=210 Gpa and m= 0.28.
(Ans: Change in length=1.75mm, change in diameter =0.0041mm)
4.A steel bar 1.2 m long, 40mm wide and 20 mm thick is subjected to an axial tensile load of 50 kN in the direction of its length. Find the change in length and thickness of the bar. Take E=200 Gpa and Poisson's ratio =0.26.
(Ans: Change in length=0.375mm, change in thickness=1.62510-3mm)
5. A metal bar 40mm40mm section, is subjected to an axial compressive load of 480 kN. The contraction of a 200 mm gauge length is found to be 0.4 mm and the increase in thickness 0.04 mm. Find Young’s Modulus and Poisson’s ratio.
(Ans: E= 150 GPa, m =0.2)

Comments

Popular posts from this blog

Relation between Modulus of Elasticity and Modulus of Rigidity

Modulus of Elasticity (E)   It is the ratio between Normal stress to Normal strain within the elastic limit. Elastic Modulus E = Normal stress/Normal strain E =  s/e Modulus of Rigidity (G)  It is the ratio between Shear stress to Shear strain within the elastic limit. Rigidity Modulus G = Shear stress/ Shear strain G =    Ƭ / ø   Relation between Modulus of Elasticity and Modulus of Rigidity: Consider a solid cube  PQRS is  subjected to a shearing force F.  Let  Ƭ     be the shear stress produced in the faces PQ and RS due to this shear force. The complementary shear stress consequently produced in the vertical faces PS and RQ is also equal to same and shown in figure as Ƭ   Due to the pure shearing force, the cube is deformed PQRS to PQR'S' . The point   S moved to S' and point R moved to R' as shown in fig.  The shear strain = The angle of distortion  ø           ...

Shearing Stresses Distribution in Circular Section

Show that the shearing stress developed at the neutral axis of a beam with circular cross section is  τ max = (4/3)(F/πr2). Assume that the shearing stress is uniformly distributed across the neutral axis.  Solution : Let us consider the circular section of a beam as displayed in following figure. We have assumed one layer EF at a distance y1 from the neutral axis of the circular section of the beam Shear stress at a section will be given by following formula as mentioned here Where, F = Shear force (N) τ = Shear stress (N/mm2) A = Area of section, where shear stress is to be determined (mm2) ȳ = Distance of C.G of the area, where shear stress is to be determined, from neutral axis of the beam section (m) Q = A. ȳ = Moment of the whole shaded area about the neutral axis I = Moment of inertia of the given section about the neutral axis (mm4) For circular cross-section, Moment of inertia, I = ПR4/4 b = Width of the given section where shear stress is to be determined. Let us co...

PORTAL METHOD and CANTILEVER METHOD

The behavior of a structure subjected to horizontal forces depends on its height to width ratio. The deformation in low-rise structures, where the height is smaller than its width, is characterized predominantly by shear deformations. In high rise building, where height is several times greater than its lateral dimensions, is dominated by bending action. To analyze the structures subjected to horizontal loading we have two methods. Portal method  and Cantilever method 1. PORTAL METHOD The portal method is an approximate analysis used for analysing building frames subjected to lateral loads such as Wind loads/ seismic forces.  Since shear deformations are dominant in low rise structures, the method makes simplifying assumptions regarding horizontal shear in columns.  Each bay of a structure is treated as a portal frame, and horizontal force is distributed equally among them. Assumptions in portal method   1. The points of inflection are located at the mid-height of e...