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Strike441 [17]
3 years ago
15

: The shaft is made of L2 tool steel, has a diameter of 40 mm, and is fixed at its ends A and B. If it is subjected to the torqu

e, determine the maximum shear stress in the bar. If the shear modulus of the steel is 75 GPa, determine the twisting angle at C.

Physics
1 answer:
Dominik [7]3 years ago
4 0

Answer:

the maximum shear stress in the bar = 9.55 MPa

the twisting angle = 0.146^0

Explanation:

From the diagram below;

Torque (T) = 2 kN × 5 mm +  2 kN × 5 mm

= 2*10^3 *0.05 + 2*10^3 *0.05

= 200 N.m

Now; If we divide the shaft into two parts AC & BC

Then :

T = T_1 + T_2 = 200          ------------ equation (1)

At the junction :

\phi _{AC} = \phi _{BC}

\phi = \frac{Tl}{GJ}

⇒ \frac{T_1 \ l_{AC}}{GJ_1}=  \frac{T_2 \ l_{BC}}{GJ_2}

T_1l_{AC} = T_2 l_{BC}

T_1*400 = T_2 * 600\\T_1 = \frac {600T_2}{400}\\T_1 = 1.5 T_2

replace T_1 = 1.5 T_2 into above equation (1)

1.5 T_2 +T_2 = 200\\2.5 T_2 = 200\\T_2 = \frac{200}{2.5}\\T_2 = 80 N.m

Again:

T_1 +T_2 = 200\\T_1 + 80 = 200\\T_1 = 200 - 80\\T_1 = 120 N.m

Now ; we can deduce that the maximum shear comes from \phi_{AC} since T_1 = 120 \ N.m

So;

\gamma_{max} = \frac{T_1 *R}{ \frac {\pi D^4}{32}}

where;

R = 20 mm

D = 40 mm = 0.04 m

Then;

\gamma_{max} = \frac{120 *20*10^{-3}}{ \frac {\pi (0.04)^4}{32}}

\gamma_{max} = 9.55 \ MPa

Thus ; the maximum shear stress in the bar = 9.55 MPa

b)

Again: \phi_c = \frac{T_1l_{AC}}{JG} =\frac{T_2l_{AC}}{JG}

\phi_c = \frac{120*0.4}{75*10^9*\pi *\frac{(0.04)^2}{32}}

\phi_c = 2.55 *10^{-3} \ rads

\phi_c = 0.146^0

Thus, the twisting angle = 0.146^0

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<h3>Center mass of the airplane</h3>

The concept of center mass of an object can be used to dtermine the mass distribution of the airplane along the line through the center.

<h3>Some assumptions</h3>
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Position of the center mass of the plane is calculated as follows;

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Learn more about center mass here: brainly.com/question/13499822

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