Question

A brass rod with a length of 1.50 m and a cross-sectional area of 2.50 cm2...

A brass rod with a length of 1.50 m and a cross-sectional area of 2.50 cm2 is fastened end to end to a nickel rod with length L and cross-sectional area 0.880 cm2 . The compound rod is subjected to equal and opposite pulls of magnitude 3.46×104 N at its ends.

a.Find the length L of the nickel rod if the elongations of the two rods are equal.

b.What is the stress in the brass rod?

c.What is the stress in the nickel rod?

d.What is the strain in the brass rod?

e.What is the strain in the nickel rod?

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Answer #1

NOTE :

Stress is defined as the force per unit area of a material.

i.e. Stress = force / cross sectional area:

sigma = rac{F}{A} ............................(1)

where,

σ = stress,

F = force applied, and

A= cross sectional area of the object.

Strain is defined as extension per unit length.

Strain has no units.

Strain = extension / original length :

  varepsilon = rac{e}{l_{0}} .................................(2)

where,

varepsilon = strain,

l0 = the original length

e = extension = (l-lo), and

l = stretched length

And the Young Modulus (E) is defined as

Stress σ E-stress- Strain

Putting the value of stress and strain , we get

E = rac{F l_{0}}{Ae} ...............................(3)

E of brass = 9.0 x 1010Pa and

E of nickel = 21 x 1010 Pa

Answer :

Given, length of brass rod = 1.5 m

cross - sectional area of brass rod = 2.50 cm2 = 2.50 x 10-4 m2

length of nickel rod = L

cross - sectional area of nickel rod = 0.880 cm2 = 0.880 x 10-4 m2

Force (F) = 3.46 x 104 N

(a)

From equation (3), we can write

e = rac{F l_{0}}{AE}

So, e_{brass} = rac{3.46 imes 10^{4} imes 1.5}{2.50 imes 10^{-4} imes 9.0 imes 10^{10}} = 23.07 imes 10^{-4}

and e_{nickel} = rac{3.46 imes 10^{4} imes L}{0.880 imes 10^{-4} imes 21 imes 10^{10}} = 18.72 imes 10^{-4} imes L

Since, elongation in brass rod = elongation in nickel rod

i.e. e_{brass} = e _{nickel}

so, 23.07 x 10-4 = 18.72 x 10-4 x L

or, L = 1.23 m

(b) Stress in brass rod :

sigma _{brass} = rac{F}{A} = rac{3.46 imes 10^{4}}{2.5 imes 10^{-4}} = 1.384 imes 10^{8} , , N/m^{2}

(c) Stress in nickel rod :

sigma _{nickel} = rac{F}{A} = rac{3.46 imes 10^{4}}{0.880 imes 10^{-4}} = 3.93 imes 10^{8} , , N/m^{2}

(d) We know that ,

  Strain = rac{Stress}{E}

or,   varepsilon = rac{sigma }{E}

So, strain in brass rod is :

  varepsilon _{brass} = rac{1.384 imes 10^{8} }{9.0 imes 10^{10}} = 15.38 imes 10^{-4}

(e) Strain in nickel rod is

  varepsilon _{nickel} = rac{3.93 imes 10^{8} }{21 imes 10^{10}} = 18.71 imes 10^{-4}

For any doubt please comment and please give an up vote. Thank you.   

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