The deflection of a uniform circular bar of diameter d and length $$l$$, which extends by an amount under a tensile pull W, when it carries the same load at its mid-span, is
A. $$\frac{{{\text{e}}l}}{{2{\text{d}}}}$$
B. $$\frac{{{{\text{e}}^2}l}}{{3{{\text{d}}^2}}}$$
C. $$\frac{{{\text{e}}{l^2}}}{{3{{\text{d}}^2}}}$$
D. $$\frac{{{{\text{e}}^{\frac{1}{2}}}}}{{3{{\text{d}}^2}}}$$
Answer: Option C
Solution (By Examveda Team)
We have a circular bar with diameter d and length l.It extends by an amount e under a tensile pull W.
We want to find the deflection when the same load W is applied at the mid-span of the bar, making it act like a beam.
1. Relate Elongation (e) to Tensile Stress and Strain:
When the bar is under a tensile pull W, we know:
Stress \( \sigma \) = Force (W) / Area (A), where \( A = \frac{\pi d^2}{4} \).
Strain \( \varepsilon \) = Change in Length (e) / Original Length (l).
Also, Stress \( \sigma \) = Young's Modulus \( E \) * Strain \( \varepsilon \).
Therefore, \( E = \frac{\sigma}{\varepsilon} \).
2. Find Young's Modulus (E) in terms of e, l, d, and W:
\( E = \frac{W}{\left( \frac{\pi d^2}{4} \right)} \div \frac{e}{l} \)
\( E = \frac{4Wl}{\pi d^2 e} \).
3. Deflection Formula for a Simply Supported Beam with a Point Load at Mid-Span:
The standard formula for the deflection (\( \delta \)) of a simply supported beam with a point load (W) at the mid-span is:
\( \delta = \frac{Wl^3}{48EI} \), where \( I \) is the area moment of inertia.
4. Area Moment of Inertia (I) for a Circular Cross-Section:
\( I = \frac{\pi d^4}{64} \).
5. Substitute I and E into the Deflection Formula:
\( \delta = \frac{Wl^3}{48 \times E \times \left( \frac{\pi d^4}{64} \right)} \)
\( \delta = \frac{Wl^3}{48 \times \left( \frac{4Wl}{\pi d^2 e} \right) \times \left( \frac{\pi d^4}{64} \right)} \)
\( \delta = \frac{Wl^3 \times \pi d^2 e \times 64}{48 \times 4Wl \times \pi d^4} \)
\( \delta = \frac{64Wl^3 \pi d^2 e}{192Wl \pi d^4} \)
\( \delta = \frac{e l^2}{3 d^2} \).
Therefore, the deflection is: \( \frac{el^2}{3d^2} \).
Correct answer: Option C \( \frac{el^2}{3d^2} \).
Join The Discussion
Comments (6)
A. $$\frac{2}{3}$$
B. $$\frac{3}{2}$$
C. $$\frac{5}{8}$$
D. $$\frac{8}{5}$$
Principal planes are subjected to
A. Normal stresses only
B. Tangential stresses only
C. Normal stresses as well as tangential stresses
D. None of these
A. $$\frac{{\text{M}}}{{\text{I}}} = \frac{{\text{R}}}{{\text{E}}} = \frac{{\text{F}}}{{\text{Y}}}$$
B. $$\frac{{\text{I}}}{{\text{M}}} = \frac{{\text{R}}}{{\text{E}}} = \frac{{\text{F}}}{{\text{Y}}}$$
C. $$\frac{{\text{M}}}{{\text{I}}} = \frac{{\text{E}}}{{\text{R}}} = \frac{{\text{F}}}{{\text{Y}}}$$
D. $$\frac{{\text{M}}}{{\text{I}}} = \frac{{\text{E}}}{{\text{R}}} = \frac{{\text{Y}}}{{\text{F}}}$$
A. $$\frac{{\text{M}}}{{\text{T}}}$$
B. $$\frac{{\text{T}}}{{\text{M}}}$$
C. $$\frac{{2{\text{M}}}}{{\text{T}}}$$
D. $$\frac{{2{\text{T}}}}{{\text{M}}}$$
can anyoe please explain thia question ??
The deflection of a uniform circular bar of diameter d and length l, which extends by an amount e under a tensile pull W, when it carries the same load at its mid-span, is:
This is the correct question
it should be length cube l³ in the answer which is wrongly given hers
For 1st case; e = WL/AE.
For the 2nd case; deflection= WL³/48EI.
I = π d^4/64 = A*d²/16 where A = πd²/4.
Def=WL³/3EAd², replacing by "e"
Now Def=eL^2/3d^2.
Qstn is not clear
Pls xplain the answr