In: Mechanical Engineering
A torsion test is performed on an aluminum probe, with the following results given in the following table:
(degress(º)) | 0 | 5 | 10 | 15 | 20 | 25 | 30 | 35 | 40 | 45 | 50 | 55 | 60 | 80 |
T kgf.m | 0 | 5 | 11 | 14 | 14.5 | 14.7 | 16.3 | 16.4 | 16.5 | 16.6 | 16.7 | 16.4 | 16.5 | 16 |
The probe dimensions are as follows:
Length(L) |
Diameter(D) |
180 | 10 |
Through your graph of behavior of shear to torsion against angular deformation determine the following:
• Limit proportional to the cut
• Shear creep (0.2% deformation)
• Maximum resistance shear • rigidity modulus (G)
• Cut Resilience Module
Failure type (malleable, ductile, tenacious or brittle)
T= torque.
J= polar moment of inertia.
for shaft J=
r= radius of shaft=0.005m.
=shear stress.
G= rigidity modulus.
= angle of twist in radians.
l= length of shaft =0.18m.
=shear strain=
From the values given for in radians.
=0 , =0.
=0.087 , =0.0024.
=0.174 , =0.0048.
=0.261 , =0.0096.
=0.349 , =0.012.
=0.523 , =0.014.
From the values given for T in Nm, in GPa.
T=0, =0.
T=49.03, =0.224.
T=107.87, =0.549.
T=137.24, =0.699.
T=142.2, =0.724
T=144.16, =0.734
T=159.85, =0.814.
(a)Limit of proportionality ,LOP is upto =0.224GPa.
(b)Shear creep(0.2% deformation) =0.725GPa.
(c)Maximum resistance shear = top point on the curve= 0.814GPa.
(d)Modulus of rigidity G= / = 0.224 */0.0024=93.33GPa.
(e)Modulus of resilance=area in the graph upto LOP =0.5*0.0024*0.224 =0.000268.