SlideShare a Scribd company logo
Torsion Testing Experiment
Introduction
Torsion is the twisting action in a member caused by two opposing moments along the longitudinal axis
of a member (see diagram below).




Practical Applications- Torsion Bars in Automobiles
This twisting can be put to good use in producing torsional
springs. “Torsion Bars” on cars are good example of use of
this idea and form a compact and simple spring system. A
long Spring steel rod or flat bar attached in such a way that
one end is anchored while the other is free to twist. One end
is fastened to the frame at one end and to a suspension part
at the other (see Figure 2). If an arm is attached at right
angles, to the free end, any movement of the arm will cause
the rod or bar to twist the bar's resistance to twisting
provides a spring action. The torsion bar replaces both Coil
spring and Leaf springs in some suspension systems.

In other cases torsion deflection can be undesirable. For instance too much twist in a car steering
column would make the car uncontrollable.
Give any other application of studying torsion?


_____________________________________________________________________________________

_____________________________________________________________________________________

_____________________________________________________________________________________
The Torsion Test
The Torsion Test allows the student to investigate the relationships between the moment (torque)
applied to a member, the material, member length and torsional deflection. Theoretically it can be
proved that:




Where:

         G = Shear Modulus (pa)
         T = Applied Torque or moment (Nm)
         J = Polar Moment of Inertia (m)
         θ = Angle of twist (rads)
         L = Effective length of member (m)


Lab Objectives
This Lab consists of two experiments. The objectives of each experiment is discussed below

    1. To twist two different materials to find shear modulus “G”, and the relationship between the
       applied moment and the angle of twist
    2. To twist a material to see how the length affects the angle of twist.

Assumptions
In our experiments we take the following assumptions:

    1. Material is homogenous
    2. Circular section remains circular and do not deform.
    3. A plane section of a material perpendicular to it's longitudinal axis remain plane and do not
       deform after the torque is applied.
    4. Shaft is loaded by a couple or torque in a plane perpendicular to the longitudinal axis of the
       plane.
    5. the torsion of the drill chucks or the cone shaped mandrels is negligible compared to the torsion
       of the test bars.
    6. There is negligible friction between the supporting rod and the chuck.
    7. Shear stress is proportional to shear strain, it means Hook's Law is applicable.
    8. In circular shafts subjected to torque shearing strain varies linearly.



         Where τ, Shearing stress in MPa,
         r = Radius of shaft in mm
         T = Twisting Moment
         J = Polar moment of inertia.
G = Modulus of rigidity.
         θ = Angle of Twist
         L = Length of the specimen

Safety Warning:
Ensure that the chucks are as tight as possible to avoid slipping.

The Equipment
The device allows the fundamental relationships of elastic deformation associated with torsion to be
measured and investigated. It is called torsion tester. In this experiment a load is applied to different
test bars and the resulting deformation measured..

The equipment consists of a loading arm with a protractor the is allowed to pivot freely and torsionally
fixed end, which can be moved up and down to give various effective lengths. Drill type chucks at each
end grip the specimen.

Accessories Provided
    1.   Measuring Tape
    2.   2 Specimen Rods (Steel, Brass)
    3.   Micrometer Screw Guage
    4.   Weight Hanger
    5.   Total 50 weights of 10g each
    6.   Chuck key
Reference Material
Some Additional Information:

       Shear Moduli:

                Steel = 79.6 GPa
                Brass = 38.0 GPa

       Nominal specimen diameter = 3 mm

                       for a circular cross section


       Where:
                D = Diameter of a section
Demo for students
The stresses caused by the torsional forces in a material are complicated. Firstly, there are shear stresses
along the axis member and secondly, there are compressive and tensile stresses at 45° to the axis. We’ll
not calculate it but simply demonstrate to proof that they exist.


Procedure for Shear Stress
    1. You are given two pieces of pipe one is solid where as the second have a slit along its length
    2. Grip and twist both pieces and compare.


What do you observe?
theslatted piece will twist easily and show the shear forces created


Procedure for Compressive and Tensile Stresses
    1. You are given a piece of ordinary circular section board chalk.
    2. Twist it gently until it breaks.

What angle does it breaks?
The chalks breaks roughly 45 degrees to the axis (forming a helix) indicating the maximum stress plane
(in tension for chalk)
LAB 1a

Objective:
   1. To prove the general torsion formulae
   2. To measure the shear modulus of material
   3. To show how torque and the material type affect the torsional deflection.

Basic Method:
   1.    Measure the diameter if the steel specimen using micrometer screw gauge.
   2.    Set the specimen length to 450 mm.
   3.    Zero the protractor using the pointer arm.
   4.    Tighten the chuck using the chuck keys.
   5.    Add masses in 50g increments to the load arm noting the angle of twist (to the nearest 0.25°) on
         the protractor until either the load arm hits the end stop or a maximum load of 500 g is used.

         Diameter of specimen rod (d) = 3 mm

         Length of Rod (L) = 450 mm

         Polar Moment of Inertia (J) = 7.95 x 10-12 m4

         Length of Lever arm (r) = 0.1m

Prove that the general torsion formula is correct


        S. No         M (g)             T (N)            Deg (°)      Θ (rad)        G= TL/J θ (GPa)

         1             50              0.049              2.5          0.044              63.61

         2             100             0.098               5           0.087              63.61

         3             150             0.147               7           0.122              68.16

         4             200             0.196              9.25         0.161              68.77

         5             250             0.245              12.5         0.218              63.61

         6             300             0.294              13.5         0.236              70.68

         7             350             0.343               16          0.279              69.58

         8             400             0.392              17.5         0.305              72.70
9           450             0.441             20             0.349           71.57

       10           500             0.491             22             0.384           72.29



Calculate Gavg



                       Gavg = 68.46GPa

Calculate Percentage Deviation of the G obtained from the G given for this material in your
textbook.
The reference given above is 79.60 Gpa where as our finding indicate it to be 68.46GPa

                                                  –



                                            –
                                                                 %

Suggest a valid reason if its greater than 5%
We have used nominal diameter rather using actual diameter due to unavailability of Micrometer Screw
Gauge
Lab 1b


Repeat the experiment for brass and note down the angular deflection against
different loads


                                                 Angular
     S. No        M (g)           T (N)       Displacement      Θ (rad)
                                               Degrees (°)
         1         50            0.04905           4          0.06981317

         2         100           0.0981            8          0.13962634

         3         150           0.14715          12.5        0.218166156

         4         200           0.1962           16.5        0.287979327

         5         250           0.24525          21          0.366519143

         6         300           0.2943           25          0.436332313

         7         350           0.34335          29          0.506145483

         8         400           0.3924          32.75        0.57159533

         9         450           0.44145          36          0.628318531
Plot a graph to determine G.

                                         Brass Loading and Displacement Curve

                                                                                              y = 1.457x
                               0.7

                               0.6
  Angular Displacement (rad)




                               0.5

                               0.4
                                                                                               Series1
                               0.3

                               0.2
                                                                                               Linear
                               0.1                                                             (Series1)
                                0
                                     0           0.1          0.2       0.3       0.4   0.5
                                                               Torque (Nm)



                                           θ = L/(GJ)*T

                                           L/(GJ) = 1.4576

                                           G = L/1.5656*J

                                           G = 38.8GPa

Discuss the value of G obtained in comparison with the value of G given in books.
Modulus of Rigidity obtained is very much close to the actual value given in books the percentage error
is calculated below

                                                                –



                                                          –
                                                                              %

Since the error is within 5% range therefore it is acceptable.

After this experiment, explain how you will determine the selection of rod if you are
constrained by the length, maximum possible deflection and maximum loading torque.
Using Modulus of Rigidity
Lab 2

Objective
         To show how the length of a member affects the torsional deflection.

Procedure
    1. Measure the diameter of the brass rod specimen using a micrometer.
    2. Set the brass specimen length to 450mm.
    3. Zero the protractor using the pointer arm.
    4. Tighten the chuck using the chuck key.
    5. Add 400 g to the load arm and
    6. Note down the angle of twist (to nearest 0.25°) on the protractor against the Length mentioned
       in the table below
    7. Decrease the length by 50 mm and note down the observations in the table below until 250mm
       is reached

Length of Lever Arm (R) = 100 mm

Diameter of the Rod (d) = 3 mm

Polar Moment of Inertia (J) = 7.95 x 10-12 m4

Mass (m)= 400 g

Calculate the Torque Applied
Applied Torque (T) = m x g x R/1000

                      = 0.3924 Nm


              S. No           Length (m)               Angle (°)                Angle (rad)

                1                   0.45                  33                      0.5760

                2                   0.4                  29.5                     0.5149

                3                   0.35                  26                      0.4538

                4                   0.3                   23                      0.4014

                5                   0.25                  20                      0.3491
Plot a graph of Angle versus Length.

                                         Angular Displacement against Length
                                0.6000
                                                                                             y = 1.134x + 0.062
                                0.5500
   Angular Displacement (rad)




                                0.5000


                                0.4500
                                                                                                   Series1
                                0.4000                                                             Linear (Series1)


                                0.3500


                                0.3000
                                         0.2   0.25   0.3      0.35      0.4   0.45    0.5
                                                            Length (m)


What do you observe?

                                As the length increases the angle of deflection increasesproportionally

Determine G using the Graph

Θ = L*(T/(GJ))

m = T/GJ = 1.1345

G = 1/m * T/J

G = 43.50 GPa

More Related Content

What's hot

Buckling test engt110
Buckling test engt110Buckling test engt110
Buckling test engt110
asghar123456
 

What's hot (20)

3 shaft stress in shafts
3 shaft   stress in shafts3 shaft   stress in shafts
3 shaft stress in shafts
 
Torsion
TorsionTorsion
Torsion
 
Shaft subjected to bending moment only (2)
Shaft subjected to bending moment only (2)Shaft subjected to bending moment only (2)
Shaft subjected to bending moment only (2)
 
Unit 2 stresses in composite sections
Unit 2  stresses in composite sectionsUnit 2  stresses in composite sections
Unit 2 stresses in composite sections
 
Bending and Torsion A.Vinoth Jebaraj
Bending and Torsion A.Vinoth JebarajBending and Torsion A.Vinoth Jebaraj
Bending and Torsion A.Vinoth Jebaraj
 
Problems on Torsion
Problems on TorsionProblems on Torsion
Problems on Torsion
 
Impact Of Jet | Jameel Academy
Impact Of Jet | Jameel AcademyImpact Of Jet | Jameel Academy
Impact Of Jet | Jameel Academy
 
Lab 8 tensile testing
Lab 8 tensile testing  Lab 8 tensile testing
Lab 8 tensile testing
 
Shafts and Shafts Components
Shafts and Shafts ComponentsShafts and Shafts Components
Shafts and Shafts Components
 
Thin and thick cylinders
Thin and thick cylindersThin and thick cylinders
Thin and thick cylinders
 
5 shaft shafts subjected to combined twisting moment and bending moment
5 shaft   shafts subjected to combined twisting moment and bending moment5 shaft   shafts subjected to combined twisting moment and bending moment
5 shaft shafts subjected to combined twisting moment and bending moment
 
Unit 2 Design Of Shafts Keys and Couplings
Unit 2 Design Of Shafts Keys and CouplingsUnit 2 Design Of Shafts Keys and Couplings
Unit 2 Design Of Shafts Keys and Couplings
 
Fluid Mechanic Lab - Venturi Meter
Fluid Mechanic Lab - Venturi MeterFluid Mechanic Lab - Venturi Meter
Fluid Mechanic Lab - Venturi Meter
 
Impact of jet
Impact of jetImpact of jet
Impact of jet
 
Lab report 1 turning
Lab report 1   turningLab report 1   turning
Lab report 1 turning
 
marcet boiler
marcet boilermarcet boiler
marcet boiler
 
Buckling test engt110
Buckling test engt110Buckling test engt110
Buckling test engt110
 
Torsion Hollow Shaft
Torsion Hollow ShaftTorsion Hollow Shaft
Torsion Hollow Shaft
 
Spring test
Spring testSpring test
Spring test
 
Torsion test machine design
Torsion test machine designTorsion test machine design
Torsion test machine design
 

Viewers also liked

Viewers also liked (8)

Introduction to Torsion
Introduction to TorsionIntroduction to Torsion
Introduction to Torsion
 
20 Ideas for your Website Homepage Content
20 Ideas for your Website Homepage Content20 Ideas for your Website Homepage Content
20 Ideas for your Website Homepage Content
 
50 Essential Content Marketing Hacks (Content Marketing World)
50 Essential Content Marketing Hacks (Content Marketing World)50 Essential Content Marketing Hacks (Content Marketing World)
50 Essential Content Marketing Hacks (Content Marketing World)
 
Prototyping is an attitude
Prototyping is an attitudePrototyping is an attitude
Prototyping is an attitude
 
10 Insightful Quotes On Designing A Better Customer Experience
10 Insightful Quotes On Designing A Better Customer Experience10 Insightful Quotes On Designing A Better Customer Experience
10 Insightful Quotes On Designing A Better Customer Experience
 
How to Build a Dynamic Social Media Plan
How to Build a Dynamic Social Media PlanHow to Build a Dynamic Social Media Plan
How to Build a Dynamic Social Media Plan
 
Learn BEM: CSS Naming Convention
Learn BEM: CSS Naming ConventionLearn BEM: CSS Naming Convention
Learn BEM: CSS Naming Convention
 
SEO: Getting Personal
SEO: Getting PersonalSEO: Getting Personal
SEO: Getting Personal
 

Similar to Torsion testing experiment (instructor)

Torsion testing experiment (student)
Torsion testing experiment (student)Torsion testing experiment (student)
Torsion testing experiment (student)
Sulaiman Dawood Barry
 
ASI Technical Reference Guide
ASI Technical Reference GuideASI Technical Reference Guide
ASI Technical Reference Guide
cshebesta
 
Transformer design
Transformer designTransformer design
Transformer design
sulaim_qais
 
070817gijyutusinnsasyoumei[1]
070817gijyutusinnsasyoumei[1]070817gijyutusinnsasyoumei[1]
070817gijyutusinnsasyoumei[1]
guest3b547c
 
Direct Shear Test
Direct Shear TestDirect Shear Test
Direct Shear Test
A K
 
[Name Sponged] Consulting Project
[Name Sponged] Consulting Project[Name Sponged] Consulting Project
[Name Sponged] Consulting Project
Ryan Elder
 
Stainless steel wire mesh
Stainless steel wire meshStainless steel wire mesh
Stainless steel wire mesh
weldmeshfence
 
Process parameters optimization for surface roughness in edm for aisi d2 steel
Process parameters optimization for surface roughness in edm for aisi d2 steelProcess parameters optimization for surface roughness in edm for aisi d2 steel
Process parameters optimization for surface roughness in edm for aisi d2 steel
IAEME Publication
 

Similar to Torsion testing experiment (instructor) (20)

Torsion testing experiment (student)
Torsion testing experiment (student)Torsion testing experiment (student)
Torsion testing experiment (student)
 
Depositiondata
DepositiondataDepositiondata
Depositiondata
 
ASI Technical Reference Guide
ASI Technical Reference GuideASI Technical Reference Guide
ASI Technical Reference Guide
 
Transformer design
Transformer designTransformer design
Transformer design
 
SPICE MODEL of 2SK3454 (Professional+BDP Model) in SPICE PARK
SPICE MODEL of 2SK3454 (Professional+BDP Model) in SPICE PARKSPICE MODEL of 2SK3454 (Professional+BDP Model) in SPICE PARK
SPICE MODEL of 2SK3454 (Professional+BDP Model) in SPICE PARK
 
070817gijyutusinnsasyoumei[1]
070817gijyutusinnsasyoumei[1]070817gijyutusinnsasyoumei[1]
070817gijyutusinnsasyoumei[1]
 
Direct Shear Test
Direct Shear TestDirect Shear Test
Direct Shear Test
 
Direct Shear Test
Direct Shear TestDirect Shear Test
Direct Shear Test
 
[Name Sponged] Consulting Project
[Name Sponged] Consulting Project[Name Sponged] Consulting Project
[Name Sponged] Consulting Project
 
kupdf.net_indian-steel-table.pdf
kupdf.net_indian-steel-table.pdfkupdf.net_indian-steel-table.pdf
kupdf.net_indian-steel-table.pdf
 
Fisica flexicion
Fisica flexicion Fisica flexicion
Fisica flexicion
 
SPICE MODEL of 2SK3454 (Standard+BDS Model) in SPICE PARK
SPICE MODEL of 2SK3454 (Standard+BDS Model) in SPICE PARKSPICE MODEL of 2SK3454 (Standard+BDS Model) in SPICE PARK
SPICE MODEL of 2SK3454 (Standard+BDS Model) in SPICE PARK
 
Stainless steel wire mesh
Stainless steel wire meshStainless steel wire mesh
Stainless steel wire mesh
 
Process parameters optimization for surface roughness in edm for aisi d2 steel
Process parameters optimization for surface roughness in edm for aisi d2 steelProcess parameters optimization for surface roughness in edm for aisi d2 steel
Process parameters optimization for surface roughness in edm for aisi d2 steel
 
Chiu i hsuan
Chiu i hsuanChiu i hsuan
Chiu i hsuan
 
SPICE MODEL of DTD123YS in SPICE PARK
SPICE MODEL of DTD123YS in SPICE PARKSPICE MODEL of DTD123YS in SPICE PARK
SPICE MODEL of DTD123YS in SPICE PARK
 
SPICE MODEL of DTD123YK in SPICE PARK
SPICE MODEL of DTD123YK in SPICE PARKSPICE MODEL of DTD123YK in SPICE PARK
SPICE MODEL of DTD123YK in SPICE PARK
 
SPICE MODEL of SSM3K102TU (Standard+BDS Model) in SPICE PARK
SPICE MODEL of SSM3K102TU (Standard+BDS Model) in SPICE PARKSPICE MODEL of SSM3K102TU (Standard+BDS Model) in SPICE PARK
SPICE MODEL of SSM3K102TU (Standard+BDS Model) in SPICE PARK
 
Bolt details
Bolt detailsBolt details
Bolt details
 
B h curve-1
B h curve-1B h curve-1
B h curve-1
 

Torsion testing experiment (instructor)

  • 1. Torsion Testing Experiment Introduction Torsion is the twisting action in a member caused by two opposing moments along the longitudinal axis of a member (see diagram below). Practical Applications- Torsion Bars in Automobiles This twisting can be put to good use in producing torsional springs. “Torsion Bars” on cars are good example of use of this idea and form a compact and simple spring system. A long Spring steel rod or flat bar attached in such a way that one end is anchored while the other is free to twist. One end is fastened to the frame at one end and to a suspension part at the other (see Figure 2). If an arm is attached at right angles, to the free end, any movement of the arm will cause the rod or bar to twist the bar's resistance to twisting provides a spring action. The torsion bar replaces both Coil spring and Leaf springs in some suspension systems. In other cases torsion deflection can be undesirable. For instance too much twist in a car steering column would make the car uncontrollable.
  • 2. Give any other application of studying torsion? _____________________________________________________________________________________ _____________________________________________________________________________________ _____________________________________________________________________________________
  • 3. The Torsion Test The Torsion Test allows the student to investigate the relationships between the moment (torque) applied to a member, the material, member length and torsional deflection. Theoretically it can be proved that: Where: G = Shear Modulus (pa) T = Applied Torque or moment (Nm) J = Polar Moment of Inertia (m) θ = Angle of twist (rads) L = Effective length of member (m) Lab Objectives This Lab consists of two experiments. The objectives of each experiment is discussed below 1. To twist two different materials to find shear modulus “G”, and the relationship between the applied moment and the angle of twist 2. To twist a material to see how the length affects the angle of twist. Assumptions In our experiments we take the following assumptions: 1. Material is homogenous 2. Circular section remains circular and do not deform. 3. A plane section of a material perpendicular to it's longitudinal axis remain plane and do not deform after the torque is applied. 4. Shaft is loaded by a couple or torque in a plane perpendicular to the longitudinal axis of the plane. 5. the torsion of the drill chucks or the cone shaped mandrels is negligible compared to the torsion of the test bars. 6. There is negligible friction between the supporting rod and the chuck. 7. Shear stress is proportional to shear strain, it means Hook's Law is applicable. 8. In circular shafts subjected to torque shearing strain varies linearly. Where τ, Shearing stress in MPa, r = Radius of shaft in mm T = Twisting Moment J = Polar moment of inertia.
  • 4. G = Modulus of rigidity. θ = Angle of Twist L = Length of the specimen Safety Warning: Ensure that the chucks are as tight as possible to avoid slipping. The Equipment The device allows the fundamental relationships of elastic deformation associated with torsion to be measured and investigated. It is called torsion tester. In this experiment a load is applied to different test bars and the resulting deformation measured.. The equipment consists of a loading arm with a protractor the is allowed to pivot freely and torsionally fixed end, which can be moved up and down to give various effective lengths. Drill type chucks at each end grip the specimen. Accessories Provided 1. Measuring Tape 2. 2 Specimen Rods (Steel, Brass) 3. Micrometer Screw Guage 4. Weight Hanger 5. Total 50 weights of 10g each 6. Chuck key
  • 5. Reference Material Some Additional Information: Shear Moduli: Steel = 79.6 GPa Brass = 38.0 GPa Nominal specimen diameter = 3 mm for a circular cross section Where: D = Diameter of a section
  • 6. Demo for students The stresses caused by the torsional forces in a material are complicated. Firstly, there are shear stresses along the axis member and secondly, there are compressive and tensile stresses at 45° to the axis. We’ll not calculate it but simply demonstrate to proof that they exist. Procedure for Shear Stress 1. You are given two pieces of pipe one is solid where as the second have a slit along its length 2. Grip and twist both pieces and compare. What do you observe? theslatted piece will twist easily and show the shear forces created Procedure for Compressive and Tensile Stresses 1. You are given a piece of ordinary circular section board chalk. 2. Twist it gently until it breaks. What angle does it breaks? The chalks breaks roughly 45 degrees to the axis (forming a helix) indicating the maximum stress plane (in tension for chalk)
  • 7. LAB 1a Objective: 1. To prove the general torsion formulae 2. To measure the shear modulus of material 3. To show how torque and the material type affect the torsional deflection. Basic Method: 1. Measure the diameter if the steel specimen using micrometer screw gauge. 2. Set the specimen length to 450 mm. 3. Zero the protractor using the pointer arm. 4. Tighten the chuck using the chuck keys. 5. Add masses in 50g increments to the load arm noting the angle of twist (to the nearest 0.25°) on the protractor until either the load arm hits the end stop or a maximum load of 500 g is used. Diameter of specimen rod (d) = 3 mm Length of Rod (L) = 450 mm Polar Moment of Inertia (J) = 7.95 x 10-12 m4 Length of Lever arm (r) = 0.1m Prove that the general torsion formula is correct S. No M (g) T (N) Deg (°) Θ (rad) G= TL/J θ (GPa) 1 50 0.049 2.5 0.044 63.61 2 100 0.098 5 0.087 63.61 3 150 0.147 7 0.122 68.16 4 200 0.196 9.25 0.161 68.77 5 250 0.245 12.5 0.218 63.61 6 300 0.294 13.5 0.236 70.68 7 350 0.343 16 0.279 69.58 8 400 0.392 17.5 0.305 72.70
  • 8. 9 450 0.441 20 0.349 71.57 10 500 0.491 22 0.384 72.29 Calculate Gavg Gavg = 68.46GPa Calculate Percentage Deviation of the G obtained from the G given for this material in your textbook. The reference given above is 79.60 Gpa where as our finding indicate it to be 68.46GPa – – % Suggest a valid reason if its greater than 5% We have used nominal diameter rather using actual diameter due to unavailability of Micrometer Screw Gauge
  • 9. Lab 1b Repeat the experiment for brass and note down the angular deflection against different loads Angular S. No M (g) T (N) Displacement Θ (rad) Degrees (°) 1 50 0.04905 4 0.06981317 2 100 0.0981 8 0.13962634 3 150 0.14715 12.5 0.218166156 4 200 0.1962 16.5 0.287979327 5 250 0.24525 21 0.366519143 6 300 0.2943 25 0.436332313 7 350 0.34335 29 0.506145483 8 400 0.3924 32.75 0.57159533 9 450 0.44145 36 0.628318531
  • 10. Plot a graph to determine G. Brass Loading and Displacement Curve y = 1.457x 0.7 0.6 Angular Displacement (rad) 0.5 0.4 Series1 0.3 0.2 Linear 0.1 (Series1) 0 0 0.1 0.2 0.3 0.4 0.5 Torque (Nm) θ = L/(GJ)*T L/(GJ) = 1.4576 G = L/1.5656*J G = 38.8GPa Discuss the value of G obtained in comparison with the value of G given in books. Modulus of Rigidity obtained is very much close to the actual value given in books the percentage error is calculated below – – % Since the error is within 5% range therefore it is acceptable. After this experiment, explain how you will determine the selection of rod if you are constrained by the length, maximum possible deflection and maximum loading torque. Using Modulus of Rigidity
  • 11. Lab 2 Objective To show how the length of a member affects the torsional deflection. Procedure 1. Measure the diameter of the brass rod specimen using a micrometer. 2. Set the brass specimen length to 450mm. 3. Zero the protractor using the pointer arm. 4. Tighten the chuck using the chuck key. 5. Add 400 g to the load arm and 6. Note down the angle of twist (to nearest 0.25°) on the protractor against the Length mentioned in the table below 7. Decrease the length by 50 mm and note down the observations in the table below until 250mm is reached Length of Lever Arm (R) = 100 mm Diameter of the Rod (d) = 3 mm Polar Moment of Inertia (J) = 7.95 x 10-12 m4 Mass (m)= 400 g Calculate the Torque Applied Applied Torque (T) = m x g x R/1000 = 0.3924 Nm S. No Length (m) Angle (°) Angle (rad) 1 0.45 33 0.5760 2 0.4 29.5 0.5149 3 0.35 26 0.4538 4 0.3 23 0.4014 5 0.25 20 0.3491
  • 12. Plot a graph of Angle versus Length. Angular Displacement against Length 0.6000 y = 1.134x + 0.062 0.5500 Angular Displacement (rad) 0.5000 0.4500 Series1 0.4000 Linear (Series1) 0.3500 0.3000 0.2 0.25 0.3 0.35 0.4 0.45 0.5 Length (m) What do you observe? As the length increases the angle of deflection increasesproportionally Determine G using the Graph Θ = L*(T/(GJ)) m = T/GJ = 1.1345 G = 1/m * T/J G = 43.50 GPa