The maximum torque that can be safely applied to a shaft of 100 mm diameter if the permissible angle of twist is 1 degree in a length of 3 m and the permissible shear stress is 30 N/mm2. Take G = 0.8 × 105 N/mm2.
4.57 kNm
This problem asks us to find the maximum torque that can be safely applied to a solid circular shaft. The safety is limited by two conditions: the maximum allowable angle of twist and the maximum allowable shear stress. We need to calculate the maximum torque permitted by each condition separately and then choose the smaller value, as that is the torque that satisfies both constraints simultaneously.
The angle of twist formula uses radians. We convert the given angle from degrees to radians:
$\theta \text{ (in radians)} = \theta \text{ (in degrees)} \times \frac{\pi}{180}$
$\theta = 1 \times \frac{\pi}{180} \text{ radians}$
For a solid circular shaft, the polar moment of inertia is given by:
$J = \frac{\pi D^4}{32}$ or $J = \frac{\pi R^4}{2}$
Using $R = 50 \text{ mm}$:
$J = \frac{\pi (50 \text{ mm})^4}{2} = \frac{\pi \times 6,250,000}{2} \text{ mm}^4 = 3,125,000 \pi \text{ mm}^4$
The torsion formula relating torque ($T$), angle of twist ($\theta$), modulus of rigidity ($G$), polar moment of inertia ($J$), and length ($L$) is:
$\frac{T}{J} = \frac{G\theta}{L}$
Rearranging for $T$:
$T_{twist} = \frac{G \theta J}{L}$
Substitute the values:
$T_{twist} = \frac{(0.8 \times 10^5 \text{ N/mm}^2) \times (\frac{\pi}{180} \text{ rad}) \times (3,125,000 \pi \text{ mm}^4)}{3000 \text{ mm}}$
$T_{twist} = \frac{0.8 \times 10^5 \times \pi^2 \times 3,125,000}{180 \times 3000} \text{ N.mm}$
$T_{twist} = \frac{0.8 \times 10^5 \times 9.8696 \times 3,125,000}{540,000} \text{ N.mm}$
$T_{twist} \approx \frac{2,467,400,000,000}{540,000} \text{ N.mm}$
$T_{twist} \approx 4,569,259 \text{ N.mm}$
Converting N.mm to kNm (1 kNm = $10^6$ N.m = $10^9$ N.mm):
$T_{twist} \approx 4,569,259 \times 10^{-9} \text{ kNm} \approx 4.569 \text{ kNm}$
Rounding to two decimal places, $T_{twist} \approx 4.57 \text{ kNm}$.
The torsion formula relating torque ($T$), shear stress ($\tau$), polar moment of inertia ($J$), and radius ($R$) is:
$\frac{T}{J} = \frac{\tau}{R}$
Rearranging for $T$:
$T_{stress} = \frac{\tau_{max} J}{R}$
Substitute the values:
$T_{stress} = \frac{(30 \text{ N/mm}^2) \times (3,125,000 \pi \text{ mm}^4)}{50 \text{ mm}}$
$T_{stress} = \frac{30 \times 3,125,000 \pi}{50} \text{ N.mm}$
$T_{stress} = 0.6 \times 3,125,000 \pi \text{ N.mm}$
$T_{stress} = 1,875,000 \pi \text{ N.mm}$
$T_{stress} \approx 1,875,000 \times 3.14159 \text{ N.mm}$
$T_{stress} \approx 5,890,487.5 \text{ N.mm}$
Converting N.mm to kNm:
$T_{stress} \approx 5,890,487.5 \times 10^{-9} \text{ kNm} \approx 5.890 \text{ kNm}$
Rounding to two decimal places, $T_{stress} \approx 5.89 \text{ kNm}$.
The shaft must satisfy both the angle of twist limit and the shear stress limit. Therefore, the maximum safe torque is the smaller of the two values calculated:
$T_{max} = \min(T_{twist}, T_{stress})$
$T_{max} = \min(4.57 \text{ kNm}, 5.89 \text{ kNm})$
$T_{max} = 4.57 \text{ kNm}$
Thus, the maximum torque that can be safely applied to the shaft is 4.57 kNm.
Which of the following assumptions are True for torsion theory for axisymmetric sections?
A tubular shaft, having an inner diameter of 30 mm and an outer diameter of 40 mm, is to be used to transmit 80 kW of power. The speed of rotation of the shaft so that the shear stress will not exceed 50 MPa is
A circular solid shaft of span L = 5 m is fixed at one end and free at the other end. A torque T = 100 kN.m is applied at the free end. The shear modulus and polar moment of inertia of the section are denoted as G and J, respectively. The torsional rigidity GJ is 50,000 kN.m2 /rad. The following are reported for this shaft:
Statement i) The rotation at the free end is 0.01 rad
Statement ii) The torsional strain energy is 1.0 kN.m
With reference to the above statements, which of the following is true?
A solid circular shaft of diameter d and length L is fixed at one end and free at the other end. A torque T is applied at the free end. The shear modulus of the material is G. The angle of twist at three free ends is