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<title>GATE Overflow for GATE XE - Recent questions in Mechanics of deformable bodies</title>
<link>https://xe.gateoverflow.in/questions/solid-mechanics/mechanics-of-deformable-bodies</link>
<description>Powered by Question2Answer</description>
<item>
<title>GATE XE 2026 | Question: 52</title>
<link>https://xe.gateoverflow.in/946/gate-xe-2026-question-52</link>
<description>At the peak (also denoted as UTS) of an engineering stress vs. engineering strain curve for ductile metal, the engineering strain is $0.2$. The corresponding true stress $(\sigma)$ vs. true strain ( $\epsilon$ ) relationship follows the equation: $\sigma=K \epsilon^{n}$, where $K$ and $n$ are constants.&lt;br /&gt;
&lt;br /&gt;
The engineering stress at the peak in $\mathrm{MPa}$ is $\_\_\_\_$ (rounded off to one decimal place).&lt;br /&gt;
&lt;br /&gt;
Given: $K=200 \mathrm{MPa}$</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/946/gate-xe-2026-question-52</guid>
<pubDate>Tue, 24 Feb 2026 15:45:43 +0000</pubDate>
</item>
<item>
<title>GATE XE 2026 | Question: 60</title>
<link>https://xe.gateoverflow.in/938/gate-xe-2026-question-60</link>
<description>&lt;p&gt;Which among the following options is/are &lt;strong&gt;CORRECT&lt;/strong&gt; unit(s) of stress?&lt;/p&gt;&lt;ol start=&quot;1&quot; style=&quot;list-style-type: upper-alpha;&quot;&gt;&lt;li&gt;$\mathrm{Nm}^{2}$&lt;/li&gt;&lt;li&gt;$\text{Pa}$&lt;/li&gt;&lt;li&gt;$\text{Nm}$&lt;/li&gt;&lt;li&gt;$\mathrm{N} / \mathrm{m}^{2}$&lt;/li&gt;&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/938/gate-xe-2026-question-60</guid>
<pubDate>Tue, 24 Feb 2026 15:44:55 +0000</pubDate>
</item>
<item>
<title>GATE XE 2026 | Question: 63</title>
<link>https://xe.gateoverflow.in/935/gate-xe-2026-question-63</link>
<description>A $\text{2D}$ state of stress at a point in a body is given by $\sigma_{x x}=-40 \mathrm{~MPa}$, $\sigma_{y y}=100 \mathrm{~MPa}$ and $\tau_{x y}=50 \mathrm{~MPa}$.&lt;br /&gt;
&lt;br /&gt;
The radius of the Mohr&amp;#039;s circle for the given state of stress is $\_\_\_\_$ $\mathrm{MPa}$ (rounded off to two decimal places).</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/935/gate-xe-2026-question-63</guid>
<pubDate>Tue, 24 Feb 2026 15:44:28 +0000</pubDate>
</item>
<item>
<title>GATE XE 2026 | Question: 64</title>
<link>https://xe.gateoverflow.in/934/gate-xe-2026-question-64</link>
<description>Sum of the principal stresses of a $\text{2D}$ stress state $\left[\begin{array}{cc}11 &amp;amp; 4 \\ 4 &amp;amp; 5\end{array}\right]$ is $\_\_\_\_$ (in integer).</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/934/gate-xe-2026-question-64</guid>
<pubDate>Tue, 24 Feb 2026 15:44:26 +0000</pubDate>
</item>
<item>
<title>GATE XE 2026 | Question: 67</title>
<link>https://xe.gateoverflow.in/931/gate-xe-2026-question-67</link>
<description>&lt;p&gt;One column with square cross section of side $r$ and another column with rectangular cross section of breadth $p$ and width $q(&amp;lt;p)$ are made from the same material. Both the columns have one end fixed, and the other end is free. They are subjected to axial loads along the centroidal axis.&lt;/p&gt;&lt;p&gt;Consider the area of cross sections of both the columns to be the same. The minimum critical Euler buckling loads of the columns with rectangular and square cross-sections are $F_{\text {rect }}$ and $F_{\mathrm{sq}}$, respectively.&lt;br&gt;&lt;br&gt;Then $\dfrac{F_{\text {rect }}}{F_{\text {sq }}}$ is $\_\_\_\_$ .&lt;/p&gt;&lt;ol start=&quot;1&quot; style=&quot;list-style-type: upper-alpha;&quot;&gt;&lt;li&gt;$\dfrac{p}{q}$&lt;/li&gt;&lt;li&gt;$\dfrac{q}{p}$&lt;/li&gt;&lt;li&gt;$\dfrac{r}{q}$&lt;/li&gt;&lt;li&gt;$\dfrac{r^{2}}{p q}$&lt;/li&gt;&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/931/gate-xe-2026-question-67</guid>
<pubDate>Tue, 24 Feb 2026 15:43:44 +0000</pubDate>
</item>
<item>
<title>GATE XE 2026 | Question: 68</title>
<link>https://xe.gateoverflow.in/930/gate-xe-2026-question-68</link>
<description>&lt;p&gt;Two prismatic rods of identical lengths are designed for the same strain energy density when subjected to the same axial load. One of the rods is made of steel (Young&#039;s modulus $=210 \mathrm{GPa}$ ) and another is made of aluminum (Young&#039;s modulus $=70 \mathrm{GPa}$).&lt;/p&gt;&lt;p&gt;If the diameter of the aluminum rod is $70$ $\mathrm{mm}$, then which one of the following options corresponds to the diameter of the steel rod in mm?&lt;/p&gt;&lt;ol start=&quot;1&quot; style=&quot;list-style-type: upper-alpha;&quot;&gt;&lt;li&gt;$53.19$&lt;/li&gt;&lt;li&gt;$70$&lt;/li&gt;&lt;li&gt;$210$&lt;/li&gt;&lt;li&gt;$29.13$&lt;/li&gt;&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/930/gate-xe-2026-question-68</guid>
<pubDate>Tue, 24 Feb 2026 15:43:40 +0000</pubDate>
</item>
<item>
<title>GATE XE 2026 | Question: 70</title>
<link>https://xe.gateoverflow.in/928/gate-xe-2026-question-70</link>
<description>&lt;p&gt;A $\text{2D}$ stress state of pure shear is shown in the figure.&lt;/p&gt;&lt;p&gt;Which one of the following options is equivalent to the given stress state?&lt;/p&gt;&lt;p&gt;Figures are not to scale.&lt;/p&gt;&lt;p style=&quot;text-align:center&quot;&gt;&lt;img alt=&quot;&quot; width=&quot;262&quot; height=&quot;256&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=13472289953150236458&quot;&gt;&lt;/p&gt;&lt;ol style=&quot;list-style-type:upper-alpha&quot;&gt;&lt;li&gt;&lt;span id=&quot;cke_bm_98S&quot; style=&quot;display: none;&quot;&gt;&amp;nbsp;&lt;/span&gt;&lt;img alt=&quot;GATE XE 2026-262&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=13996735461166491738&quot;&gt;&lt;/li&gt;&lt;li&gt;&lt;img alt=&quot;GATE XE 2026-262&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=9275912779185703572&quot;&gt;&lt;/li&gt;&lt;li&gt;&lt;img alt=&quot;GATE XE 2026-262&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=12317468977400916956&quot;&gt;&lt;/li&gt;&lt;li&gt;&lt;img alt=&quot;GATE XE 2026-262&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=9684364378207285685&quot;&gt;&lt;/li&gt;&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/928/gate-xe-2026-question-70</guid>
<pubDate>Tue, 24 Feb 2026 15:43:02 +0000</pubDate>
</item>
<item>
<title>GATE XE 2026 | Question: 73</title>
<link>https://xe.gateoverflow.in/925/gate-xe-2026-question-73</link>
<description>&lt;p&gt;The bending moment diagram for a simply supported beam is piecewise linear as shown in the figure. The bending moment $M(\mathrm{x})$ at $\mathrm{x}=0.5 \mathrm{~m}$ is $5$ $\mathrm{Nm}$. The beam has a rectangular cross-section with an area of $1 \mathrm{~m}^{2}$.&lt;br&gt;&lt;br&gt;The absolute value of the maximum shear stress on the cross-section at $x=0.75 \mathrm{~m}$ is $\_\_\_\_$ $\mathrm{N} / \mathrm{m}^{2}$ (in integer).&lt;br&gt; &lt;/p&gt;&lt;p style=&quot;text-align:center&quot;&gt;&lt;img alt=&quot;&quot; width=&quot;477&quot; height=&quot;267&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=453460113578579553&quot;&gt;&lt;/p&gt;&lt;p&gt; &lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/925/gate-xe-2026-question-73</guid>
<pubDate>Tue, 24 Feb 2026 15:42:39 +0000</pubDate>
</item>
<item>
<title>GATE XE 2026 | Question: 74</title>
<link>https://xe.gateoverflow.in/924/gate-xe-2026-question-74</link>
<description>A thin walled cylindrical container of diameter $2$ $\mathrm{m}$ and wall thickness of $2.5$ $\mathrm{cm}$ is made of steel whose Young&amp;#039;s modulus is $200$ $\mathrm{GPa}$ and yield stress is $450$ $\mathrm{MPa}$.&lt;br /&gt;
&lt;br /&gt;
Using von Mises criteria, the maximum permissible pressure is $\_\_\_\_$ $\mathrm{MPa}$ (rounded off to the nearest integer).</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/924/gate-xe-2026-question-74</guid>
<pubDate>Tue, 24 Feb 2026 15:42:26 +0000</pubDate>
</item>
<item>
<title>GATE XE 2026 | Question: 75</title>
<link>https://xe.gateoverflow.in/923/gate-xe-2026-question-75</link>
<description>A solid axial bar made of steel with Young&amp;#039;s modulus, $200$ $\mathrm{GPa}$ and Poisson&amp;#039;s ratio, $0.3$, is subjected to uniaxial stress of $50$ $\mathrm{MPa}$.&lt;br /&gt;
&lt;br /&gt;
The absolute value of the maximum shear strain on the outer surface of the bar is $\_\_\_\_$ $\times 10^{-4}$ (rounded off to two decimal places).</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/923/gate-xe-2026-question-75</guid>
<pubDate>Tue, 24 Feb 2026 15:42:25 +0000</pubDate>
</item>
<item>
<title>GATE XE 2026 | Question: 76</title>
<link>https://xe.gateoverflow.in/922/gate-xe-2026-question-76</link>
<description>&lt;p&gt;$\text{EFGH}$ (solid lines) is the initial configuration and $\mathrm{E}^{\prime} \mathrm{F}^{\prime} \mathrm{G}^{\prime} \mathrm{H}^{\prime}$ (dashed lines) is the deformed configuration of an object as shown in the figure. $\mathrm{E}^{\prime}$ coincides with $\text{E}$ and $\mathrm{F}^{\prime}$ coincides with $\text{F}$.&lt;/p&gt;&lt;p&gt;The average normal strain along the line segment $\text{OP}$ is $\_\_\_\_$ (rounded off to three decimal places).&lt;/p&gt;&lt;p style=&quot;text-align:center&quot;&gt;&lt;img alt=&quot;&quot; width=&quot;400&quot; height=&quot;292&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=14953455683059306282&quot;&gt;&lt;/p&gt;&lt;p&gt;&lt;br&gt;&lt;br&gt;Figure is not to scale.&lt;br&gt;All units are in $\mathrm{mm}$.&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/922/gate-xe-2026-question-76</guid>
<pubDate>Tue, 24 Feb 2026 15:42:24 +0000</pubDate>
</item>
<item>
<title>GATE XE 2026 | Question: 77</title>
<link>https://xe.gateoverflow.in/921/gate-xe-2026-question-77</link>
<description>&lt;p&gt;A simply supported beam of length $l=2 \mathrm{~m}$ is subjected to a concentrated moment $M=150 \mathrm{~kNm}$ at a distance $l / 2$ from the left end as shown in the figure. The elastic-strain energy $U$ of the beam is given by the following expression:&lt;/p&gt;&lt;p&gt;$$U=\frac{M^{2} l}{48 E I}$$&lt;/p&gt;&lt;p&gt;The section modulus of the beam is $E I=25 \times 10^{5} \mathrm{Nm}^{2}$.&lt;/p&gt;&lt;p&gt;The absolute value of the slope of the beam at a distance $l / 2$ from the left end is $\_\_\_\_$ (rounded off to three decimal places).&lt;br&gt;&lt;br&gt; &lt;/p&gt;&lt;p style=&quot;text-align:center&quot;&gt;&lt;img alt=&quot;&quot; width=&quot;560&quot; height=&quot;248&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=14035830531018860792&quot;&gt;&lt;/p&gt;&lt;p&gt; &lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/921/gate-xe-2026-question-77</guid>
<pubDate>Tue, 24 Feb 2026 15:42:21 +0000</pubDate>
</item>
<item>
<title>GATE XE 2026 | Question: 118</title>
<link>https://xe.gateoverflow.in/880/gate-xe-2026-question-118</link>
<description>A rectangular plastic specimen with a cross-sectional area of $240 \mathrm{~mm}^{2}$ is subjected to tension with a force of $15000$ $\mathrm{N}$ resulting in elastic deformation. If the Young&amp;#039;s modulus of the specimen is $34.55$ $\mathrm{MPa}$, the value of strain is $\_\_\_\_\_\_$ (rounded off to two decimal places).</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/880/gate-xe-2026-question-118</guid>
<pubDate>Tue, 24 Feb 2026 15:32:58 +0000</pubDate>
</item>
<item>
<title>GATE XE 2025 | Question: 66</title>
<link>https://xe.gateoverflow.in/724/gate-xe-2025-question-66</link>
<description>&lt;p&gt;Consider a spring-mass system with mass $m$ and spring stiffness $k$ as shown in the illustration. At time $t=0$, the mass is displaced by $P$ units and the velocity of the mass is zero. The displacement of the mass, $x(t)$, is measured from the equilibrium position.&lt;/p&gt;

&lt;p&gt;Which one of the following functions represent $x(t)$?&lt;/p&gt;

&lt;p&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=11207778461545633322&quot;&gt;&lt;/p&gt;

&lt;ol start=&quot;1&quot; style=&quot;list-style-type:upper-alpha&quot;&gt;
	&lt;li&gt;$P \cos \left(\sqrt{\frac{k}{m}} t\right)+P \sin \left(\sqrt{\frac{k}{m}} t\right)$&lt;/li&gt;
	&lt;li&gt;$P \sin \left(\sqrt{\frac{k}{m}} t\right)$&lt;/li&gt;
	&lt;li&gt;$\frac{P}{2} \cos \left(\sqrt{\frac{k}{m}} t\right)+\frac{P}{2} \sin \left(\sqrt{\frac{k}{m}} t\right)$&lt;/li&gt;
	&lt;li&gt;$P \cos \left(\sqrt{\frac{k}{m}} t\right)$&lt;/li&gt;
&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/724/gate-xe-2025-question-66</guid>
<pubDate>Sun, 04 May 2025 19:06:53 +0000</pubDate>
</item>
<item>
<title>GATE XE 2025 | Question: 68</title>
<link>https://xe.gateoverflow.in/722/gate-xe-2025-question-68</link>
<description>&lt;p&gt;​​​​The Mohr&#039;s circle corresponding to an infinitesimal element is shown in the figure. The plane $\text{PQ}$&amp;nbsp;in the infinitesimal element, at an angle of $\theta$ from the $x$-axis, is in a state of pure shear.&lt;/p&gt;

&lt;p&gt;Which one of the following values of $\theta$ (in degrees) is CORRECT?&lt;/p&gt;

&lt;p&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=2518621683064907241&quot;&gt;&lt;/p&gt;

&lt;ol start=&quot;1&quot; style=&quot;list-style-type:upper-alpha&quot;&gt;
	&lt;li&gt;$90$&lt;/li&gt;
	&lt;li&gt;$60$&lt;/li&gt;
	&lt;li&gt;$45$&lt;/li&gt;
	&lt;li&gt;$120$&lt;/li&gt;
&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/722/gate-xe-2025-question-68</guid>
<pubDate>Sun, 04 May 2025 19:06:48 +0000</pubDate>
</item>
<item>
<title>GATE XE 2025 | Question: 69</title>
<link>https://xe.gateoverflow.in/721/gate-xe-2025-question-69</link>
<description>&lt;p&gt;The two-dimensional state of stress, in an infinitesimal element, is given by&lt;/p&gt;

&lt;p&gt;$\sigma_{x x}=800 \mathrm{MPa}, \sigma_{x y}=300 \mathrm{MPa}$ and $\sigma_{y y}=0 \mathrm{MPa}$.&lt;/p&gt;

&lt;p&gt;Which one of the following options is the maximum shear stress (in $\mathrm{MPa}$) in the element?&lt;/p&gt;

&lt;ol start=&quot;1&quot; style=&quot;list-style-type:upper-alpha&quot;&gt;
	&lt;li&gt;$500$&lt;/li&gt;
	&lt;li&gt;$400$&lt;/li&gt;
	&lt;li&gt;$800$&lt;/li&gt;
	&lt;li&gt;$300$&lt;/li&gt;
&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/721/gate-xe-2025-question-69</guid>
<pubDate>Sun, 04 May 2025 19:06:46 +0000</pubDate>
</item>
<item>
<title>GATE XE 2025 | Question: 72</title>
<link>https://xe.gateoverflow.in/718/gate-xe-2025-question-72</link>
<description>&lt;p&gt;Consider a beam with a square box cross-section as shown in the figure. The outer square has a length of $10 \: \mathrm{mm}$. The thickness of the section is $1&amp;nbsp;\: \mathrm{mm}$.&lt;/p&gt;

&lt;p&gt;The area moment of inertia about the $x$-axis is $\_\_\_\_\_\_ \: \mathrm{mm}^{4}$ (in integer).&lt;/p&gt;

&lt;p&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=55094374112293366&quot;&gt;&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/718/gate-xe-2025-question-72</guid>
<pubDate>Sun, 04 May 2025 19:06:39 +0000</pubDate>
</item>
<item>
<title>GATE XE 2025 | Question: 73</title>
<link>https://xe.gateoverflow.in/717/gate-xe-2025-question-73</link>
<description>&lt;p&gt;For a certain linear elastic isotropic material, the Young&#039;s modulus is $140 \: \mathrm{GPa}$ and the shear modulus is $50 \: \mathrm{GPa}$.&lt;/p&gt;

&lt;p&gt;The Poisson&#039;s ratio for the material is $\_\_\_\_\_\_$ (&lt;em&gt;rounded off up to two decimal places&lt;/em&gt;).&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/717/gate-xe-2025-question-73</guid>
<pubDate>Sun, 04 May 2025 19:06:38 +0000</pubDate>
</item>
<item>
<title>GATE XE 2025 | Question: 76</title>
<link>https://xe.gateoverflow.in/714/gate-xe-2025-question-76</link>
<description>&lt;p&gt;​​​​Which one of the following vertical columns, of circular cross-section, sustains the highest load without buckling?&lt;/p&gt;

&lt;ol start=&quot;1&quot; style=&quot;list-style-type:upper-alpha&quot;&gt;
	&lt;li&gt;Cantilever column with a length $\text{L}$ and cross-section diameter $\text{d}$&lt;/li&gt;
	&lt;li&gt;Column with hinge at one end and roller at the other end with a length $2 \:\text{L}$&amp;nbsp;and cross-section diameter $\text{d}$.&lt;/li&gt;
	&lt;li&gt;Cantilever column with a length $\text{L}$&amp;nbsp;and cross-section diameter $2\:\text{d}$&lt;/li&gt;
	&lt;li&gt;Column with hinge at one end and roller at the other end with a length&amp;nbsp;$\text{L}$ and cross-section diameter $\text{d}$.&lt;/li&gt;
&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/714/gate-xe-2025-question-76</guid>
<pubDate>Sun, 04 May 2025 19:06:33 +0000</pubDate>
</item>
<item>
<title>GATE XE 2025 | Question: 79</title>
<link>https://xe.gateoverflow.in/711/gate-xe-2025-question-79</link>
<description>&lt;p&gt;A closed thin cylindrical tank with a mean diameter $\mathrm{d}=300 \mathrm{~mm}$ and thickness $\mathrm{t}=2 \mathrm{~mm}$, is subjected to a uniform internal gas pressure $p$. The allowable shear stress on the curved wall of the tank is $70 \: \mathrm{MPa}$.&lt;/p&gt;

&lt;p&gt;Based on the Tresca criteria, which one of the following options for the maximum safe value of $p$ (in $\mathrm{MPa}$) is CORRECT?&lt;/p&gt;

&lt;ol start=&quot;1&quot; style=&quot;list-style-type:upper-alpha&quot;&gt;
	&lt;li&gt;$3.73$&lt;/li&gt;
	&lt;li&gt;$7.46$&lt;/li&gt;
	&lt;li&gt;$1.87$&lt;/li&gt;
	&lt;li&gt;$5.60$&lt;/li&gt;
&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/711/gate-xe-2025-question-79</guid>
<pubDate>Sun, 04 May 2025 19:06:25 +0000</pubDate>
</item>
<item>
<title>GATE XE 2025 | Question: 80</title>
<link>https://xe.gateoverflow.in/710/gate-xe-2025-question-80</link>
<description>&lt;p&gt;​​​An infinitesimal square element $\text{PQRS}$ is shown in the figure. The $x$ and $y$ axes are also marked in the figure. The strains on the element are given by&lt;/p&gt;

&lt;p&gt;$\varepsilon_{x x}=500 \times 10^{-6}, \: \varepsilon_{y y}=100 \times 10^{-6} \text { and } \varepsilon_{x y}=0$&lt;/p&gt;

&lt;p&gt;Which of the following statements is/are $\textsf{CORRECT}$?&lt;/p&gt;

&lt;p&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=16469368682632368151&quot;&gt;&lt;/p&gt;

&lt;ol start=&quot;1&quot; style=&quot;list-style-type:upper-alpha&quot;&gt;
	&lt;li&gt;Percentage change in length of the diagonal $\text{PR}$ is $0.03$.&lt;/li&gt;
	&lt;li&gt;Change in angle between $\text{PR}$ and $\text{QS}$ is $4 \times 10^{-4} \: \mathrm{rad}$.&lt;/li&gt;
	&lt;li&gt;Change in angle between $\text{PR}$ and $\text{QS}$ is $2 \times 10^{-4} \: \mathrm{rad}$.&lt;/li&gt;
	&lt;li&gt;Percentage change in length of the diagonal $\text{QS}$ is $0.03$.&lt;/li&gt;
&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/710/gate-xe-2025-question-80</guid>
<pubDate>Sun, 04 May 2025 19:06:22 +0000</pubDate>
</item>
<item>
<title>GATE XE 2025 | Question: 81</title>
<link>https://xe.gateoverflow.in/709/gate-xe-2025-question-81</link>
<description>&lt;p&gt;The figure shows the stress distribution across an internal surface of a rectangular beam of height $30 \: \mathrm{mm}$ and depth $10 \: \mathrm{mm}$. The normal stress distribution is given by the expression $\sigma_{x x}=200 y+500 \mathrm{~N} / \mathrm{mm}^{2} ; y$ is the distance in $\mathrm{mm}$ from the centroidal axis of the beam. Assume that there is no variation in the stress distribution along the $z$ -direction.&lt;/p&gt;

&lt;p&gt;Which of the following statements is/are $\textsf{CORRECT}$?&lt;/p&gt;

&lt;p&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=1770040557786444339&quot;&gt;&lt;/p&gt;

&lt;ol start=&quot;1&quot; style=&quot;list-style-type:upper-alpha&quot;&gt;
	&lt;li&gt;The net force in the $x$ direction is $150 \: \mathrm{kN}$.&lt;/li&gt;
	&lt;li&gt;The net force in the $x$ direction is $75 \: \mathrm{kN}$.&lt;/li&gt;
	&lt;li&gt;The net moment about the $z$ axis is $4500\: \mathrm{Nm}$.&lt;/li&gt;
	&lt;li&gt;The net moment about the $z$ axis is $2250 \: \mathrm{Nm}$.&lt;/li&gt;
&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/709/gate-xe-2025-question-81</guid>
<pubDate>Sun, 04 May 2025 19:06:19 +0000</pubDate>
</item>
<item>
<title>GATE XE 2025 | Question: 82</title>
<link>https://xe.gateoverflow.in/708/gate-xe-2025-question-82</link>
<description>A vertical column fixed at one end is subjected to a compressive axial load at the free end. The column&amp;#039;s section modulus, $\text{EI}$, is $9.82 \times 10^{5} \: \mathrm{Nm}^{2}$ and the cross-section area is $7.85 \times 10^{-3} \mathrm{~m}^{2}$. The length of the column is $2 \: \mathrm{m}$. The yield stress of the material is $145 \: \mathrm{MPa}$.&lt;br /&gt;
&lt;br /&gt;
If the column can fail either in buckling or by Tresca&amp;#039;s criterion, the maximum load that the structure can safely sustain is $\_\_\_\_\_\_ \: \mathrm{kN}$ (rounded off to one decimal place).</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/708/gate-xe-2025-question-82</guid>
<pubDate>Sun, 04 May 2025 19:06:16 +0000</pubDate>
</item>
<item>
<title>GATE XE 2025 | Question: 83</title>
<link>https://xe.gateoverflow.in/707/gate-xe-2025-question-83</link>
<description>&lt;p&gt;A simply-supported beam, with a point load $\text{P}=150 \: \mathrm{kN}$ at a distance of $\text{L} / 3$ from the left end, is shown in the figure. The elastic-strain energy $\text{(U)}$ of the beam is given by the following expression:&lt;/p&gt;

&lt;p&gt;$$\mathrm{U}=\frac{2}{243} \frac{\mathrm{P}^{2} \mathrm{~L}^{3}}{\mathrm{EI}}$$&lt;/p&gt;

&lt;p&gt;where the section modulus, $\mathrm{EI}$, is $16.66 \times 10^{5} \: \mathrm{Nm}^{2}$ and the length of the beam $\mathrm{L}$ is $1 \: \mathrm{m}$.&lt;/p&gt;

&lt;p&gt;The deflection at the loading point is $\_\_\_\_\_\_\_$ mm (rounded off to two decimal places).&lt;/p&gt;

&lt;p&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=1482338902901448523&quot;&gt;&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/707/gate-xe-2025-question-83</guid>
<pubDate>Sun, 04 May 2025 19:06:15 +0000</pubDate>
</item>
<item>
<title>GATE XE 2025 | Question: 84</title>
<link>https://xe.gateoverflow.in/706/gate-xe-2025-question-84</link>
<description>&lt;p&gt;A simply-supported beam has a circular cross-section with a diameter of $20 \: \mathrm{mm}$ , area of $314.2 \mathrm{~mm}^{2}$, area moment of inertia of $7854 \mathrm{~mm}^{4}$ and a length $\text{L}$ of $4 \: \mathrm{m}$ . A point load $\mathrm{P}=100 \mathrm{~N}$ acts at the center and an axial load $\mathrm{Q}=20 \mathrm{kN}$ acts through the centroidal axis as shown in the figure.&lt;/p&gt;

&lt;p&gt;The magnitude of the offset between the neutral axis and the centroidal axis, at $\mathrm{L} / 2$ from the left, is $\_\_\_\_\_\_$ mm (rounded off to one decimal place).&lt;/p&gt;

&lt;p&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=12465989925536379745&quot;&gt;&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/706/gate-xe-2025-question-84</guid>
<pubDate>Sun, 04 May 2025 19:06:13 +0000</pubDate>
</item>
<item>
<title>GATE XE 2025 | Question: 87</title>
<link>https://xe.gateoverflow.in/703/gate-xe-2025-question-87</link>
<description>&lt;p&gt;A bar of length $\text{L}=1 \mathrm{~m}$ is fixed at one end. Before heating its free end has a gap of $\delta=0.1 \mathrm{~mm}$ from a rigid wall as shown in the figure. Now the bar is heated resulting in a uniform temperature rise of $10^{\circ} \mathrm{C}$. The coefficient of linear thermal expansion of the material is $20 \times 10^{-6} /{ }^{\circ} \mathrm{C}$ and the Young&#039;s modulus of elasticity is $100 \: \mathrm{GPa}$. Assume that the material properties do not change with temperature.&lt;/p&gt;

&lt;p&gt;The magnitude of the resulting axial stress on the bar is $\_\_\_\_\_\_ \: \mathrm{&amp;nbsp;MPa}$ (in integer).&lt;/p&gt;

&lt;p&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=16575869893123084500&quot;&gt;&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/703/gate-xe-2025-question-87</guid>
<pubDate>Sun, 04 May 2025 19:06:09 +0000</pubDate>
</item>
<item>
<title>GATE XE 2025 | Question: 122</title>
<link>https://xe.gateoverflow.in/668/gate-xe-2025-question-122</link>
<description>&lt;p&gt;​​​During material testing, stress is applied from time $t_{i}$ to $t_{f}$ as shown below:&lt;/p&gt;

&lt;p&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=5642170303997014359&quot;&gt;&lt;/p&gt;

&lt;p&gt;The corresponding strain responses for three different materials are shown in plots $\mathbf{P}, \mathbf{Q}$ and $\mathbf{R}$.&lt;/p&gt;

&lt;p&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=12429730910037919674&quot;&gt;&lt;/p&gt;

&lt;p&gt;Choose the option(s) where the strain response is correctly mapped to its material class.&lt;/p&gt;

&lt;ol start=&quot;1&quot; style=&quot;list-style-type:upper-alpha&quot;&gt;
	&lt;li&gt;$\text{P}$- purely elastic; $\text{Q}$- purely viscous; $\text{R}$- viscoelastic&lt;/li&gt;
	&lt;li&gt;$\text{P}$- purely elastic; $\text{Q}$- viscoelastic; $\text{R}$- purely viscous&lt;/li&gt;
	&lt;li&gt;$\text{P}$- purely viscous; $\text{Q}$- purely elastic; $\text{R}$- viscoelastic&lt;/li&gt;
	&lt;li&gt;$\text{P}$- purely viscous; $\text{Q}$- viscoelastic; $\text{R}$- purely elastic&lt;/li&gt;
&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/668/gate-xe-2025-question-122</guid>
<pubDate>Sun, 04 May 2025 19:04:54 +0000</pubDate>
</item>
<item>
<title>GATE XE 2024 | Question: 35</title>
<link>https://xe.gateoverflow.in/381/gate-xe-2024-question-35</link>
<description>&lt;p&gt;Mechanical behaviour of a crystalline ceramic material is best described as&lt;/p&gt;

&lt;ol style=&quot;list-style-type:upper-alpha&quot;&gt;
	&lt;li&gt;ductile&lt;/li&gt;
	&lt;li&gt;brittle&lt;/li&gt;
	&lt;li&gt;viscoelastic&lt;/li&gt;
	&lt;li&gt;Viscoplastic
	&lt;p&gt;&amp;nbsp;&lt;/p&gt;
	&lt;/li&gt;
&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/381/gate-xe-2024-question-35</guid>
<pubDate>Sun, 21 Jul 2024 16:42:18 +0000</pubDate>
</item>
<item>
<title>GATE XE 2024 | Question: 56</title>
<link>https://xe.gateoverflow.in/360/gate-xe-2024-question-56</link>
<description>&lt;p&gt;The engineering stress $(\sigma)$ vs. engineering strain $(\varepsilon)$ curve obtained by conducting uniaxial tension test on a steel specimen is shown in the figure $\text{(the sketched curve is not to the scale)}$. The specimen exhibits cup-and-cone failure within its gage length. Which point on the curve corresponds to the beginning of necking in the test specimen?&lt;/p&gt;

&lt;p&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=10490914305406535778&quot; width=&quot;400&quot;&gt;&lt;/p&gt;

&lt;ol style=&quot;list-style-type:upper-alpha&quot;&gt;
	&lt;li&gt;P&lt;/li&gt;
	&lt;li&gt;Q&lt;/li&gt;
	&lt;li&gt;R&lt;/li&gt;
	&lt;li&gt;S
	&lt;p&gt;&amp;nbsp;&lt;/p&gt;
	&lt;/li&gt;
&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/360/gate-xe-2024-question-56</guid>
<pubDate>Sun, 21 Jul 2024 16:42:01 +0000</pubDate>
</item>
<item>
<title>GATE XE 2024 | Question: 59</title>
<link>https://xe.gateoverflow.in/357/gate-xe-2024-question-59</link>
<description>&lt;p&gt;&amp;nbsp;&lt;/p&gt;

&lt;p&gt;A mass $M$ is hung from a frictionless, massless pulley. The pulley is suspended by using an inextensible, massless rope of which one end is directly fixed to a support, and the other end is connected to the support through a linear spring of stiffness constant $k$ $\text{(see figure)}$. The natural frequency of this system is&lt;/p&gt;

&lt;p style=&quot;text-align:center&quot;&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=13599943474839353375&quot; width=&quot;200&quot;&gt;&lt;/p&gt;

&lt;p&gt;&amp;nbsp;&lt;/p&gt;

&lt;ol style=&quot;list-style-type:upper-alpha&quot;&gt;
	&lt;li&gt;$\sqrt{\frac{4 k}{M}}$&lt;/li&gt;
	&lt;li&gt;$\sqrt{\frac{2 k}{M}}$&lt;/li&gt;
	&lt;li&gt;$\sqrt{\frac{k}{M}}$&lt;/li&gt;
	&lt;li&gt;$\sqrt{\frac{k}{2M}}$&lt;/li&gt;
&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/357/gate-xe-2024-question-59</guid>
<pubDate>Sun, 21 Jul 2024 16:41:58 +0000</pubDate>
</item>
<item>
<title>GATE XE 2024 | Question: 60</title>
<link>https://xe.gateoverflow.in/356/gate-xe-2024-question-60</link>
<description>&lt;p&gt;A simply-supported beam of rectangular cross-section $\text{(width $w$ and height $h$)}$ is subjected to the loads as shown in the figure $\text{(i)}$. The enlarged view of the beam cross-section is shown in figure $\text{(ii)}$. The coordinate system is indicated in the figures. Assuming Euler-Bernoulli beam approximation, the shear stress $\tau_{x z}$ and normal stress $\sigma_{x x}$ at the origin, $\text{O}$ are respectively given by&lt;/p&gt;

&lt;p&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=8764682112226828001&quot; width=&quot;500&quot;&gt;&lt;/p&gt;

&lt;p&gt;&amp;nbsp;&lt;/p&gt;

&lt;ol style=&quot;list-style-type:upper-alpha&quot;&gt;
	&lt;li&gt;$\frac{3 P}{2 w h}, \frac{3 P L}{2 w h^{2}}$&lt;/li&gt;
	&lt;li&gt;$0, \frac{3 P L}{2 w h^{2}}$&lt;/li&gt;
	&lt;li&gt;$\frac{3 P}{2 w h}, 0$&lt;/li&gt;
	&lt;li&gt;$0,0$
	&lt;p&gt;&amp;nbsp;&lt;/p&gt;
	&lt;/li&gt;
&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/356/gate-xe-2024-question-60</guid>
<pubDate>Sun, 21 Jul 2024 16:41:57 +0000</pubDate>
</item>
<item>
<title>GATE XE 2024 | Question: 62</title>
<link>https://xe.gateoverflow.in/354/gate-xe-2024-question-62</link>
<description>&lt;p&gt;A solid circular shaft of diameter $100$ mm is subjected to a torque $3 \pi \mathrm{kNm}$. Which of the following statements about the state of stress in the shaft is/are correct?&lt;/p&gt;

&lt;ol style=&quot;list-style-type:upper-alpha&quot;&gt;
	&lt;li&gt;The maximum shear stress is $48$ MPa&lt;/li&gt;
	&lt;li&gt;The maximum tensile stress is $48$ MPa&lt;/li&gt;
	&lt;li&gt;The magnitude of maximum compressive stress is $48$ MPa&lt;/li&gt;
	&lt;li&gt;The magnitude of shear stress is $48$ MPa at all points in the shaft
	&lt;p&gt;&amp;nbsp;&lt;/p&gt;
	&lt;/li&gt;
&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/354/gate-xe-2024-question-62</guid>
<pubDate>Sun, 21 Jul 2024 16:41:55 +0000</pubDate>
</item>
<item>
<title>GATE XE 2024 | Question: 63</title>
<link>https://xe.gateoverflow.in/353/gate-xe-2024-question-63</link>
<description>&lt;p&gt;&amp;nbsp;&lt;/p&gt;

&lt;p&gt;A spring is connected to an elastic bar as shown in the figure. The spring has a stiffness constant of $10^{7} \mathrm{~N} / \mathrm{m}$. The bar is 70 mm long, and has an area of crosssection $10 \mathrm{~mm}^{2}$. The Young&#039;s modulus of the bar material is $70,000 \mathrm{MPa}$. A force $F=5000 \mathrm{~N}$ is applied at point $O$ along the axis of the bar and the spring. The resulting deflection of Point $O$ in mm $\text{(rounded to one decimal place)}$ is ___________.&lt;/p&gt;

&lt;p style=&quot;text-align:center&quot;&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=10376381536885311700&quot; width=&quot;400&quot;&gt;&lt;/p&gt;

&lt;p&gt;&amp;nbsp;&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/353/gate-xe-2024-question-63</guid>
<pubDate>Sun, 21 Jul 2024 16:41:55 +0000</pubDate>
</item>
<item>
<title>GATE XE 2024 | Question: 69</title>
<link>https://xe.gateoverflow.in/347/gate-xe-2024-question-69</link>
<description>&lt;p&gt;A critical point on a component is subjected to the state of stress $[\sigma]$ as given in the following. The yield strength of the material is $400$ MPa . By considering maximum shear stress $\text{(Tresca)}$ theory, the possible value(s) of $\sigma_{0}$ at the onset of yielding is/are,&lt;br&gt;
\[&lt;br&gt;
[\sigma]=\left[\begin{array}{ccc}&lt;br&gt;
280 &amp;amp; 0 &amp;amp; 0 \\&lt;br&gt;
0 &amp;amp; \sigma_{o} &amp;amp; 0 \\&lt;br&gt;
0 &amp;amp; 0 &amp;amp; -60&lt;br&gt;
\end{array}\right] \mathrm{MPa}&lt;br&gt;
\]&lt;/p&gt;

&lt;ol style=&quot;list-style-type:upper-alpha&quot;&gt;
	&lt;li&gt;$340$&lt;/li&gt;
	&lt;li&gt;$680$&lt;/li&gt;
	&lt;li&gt;$-120$&lt;/li&gt;
	&lt;li&gt;$-460$
	&lt;p&gt;&amp;nbsp;&lt;/p&gt;
	&lt;/li&gt;
&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/347/gate-xe-2024-question-69</guid>
<pubDate>Sun, 21 Jul 2024 16:41:48 +0000</pubDate>
</item>
<item>
<title>GATE XE 2024 | Question: 70</title>
<link>https://xe.gateoverflow.in/346/gate-xe-2024-question-70</link>
<description>&lt;p&gt;A plane passing through a point $\text{Q}$ inside a body is shown. The unit normal of the plane is $\hat{n}=0.6 \hat{\imath}+0.8 \hat{\jmath}$, as shown in the figure. The traction (stress) vector on the plane at point $\text{Q}$ is given by $\vec{t}=(50 \hat{\imath}+20 \hat{\jmath}) \mathrm{MPa}$. Given that at point Q , $\sigma_{x x}=\sigma_{y y}$, the shear stress component $\tau_{x y}$ $\text{(in MPa, rounded off to two decimal places)}$ is _________.&lt;/p&gt;

&lt;p style=&quot;text-align:center&quot;&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=9417931771201714572&quot; width=&quot;400&quot;&gt;&lt;/p&gt;

&lt;p&gt;&amp;nbsp;&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/346/gate-xe-2024-question-70</guid>
<pubDate>Sun, 21 Jul 2024 16:41:48 +0000</pubDate>
</item>
<item>
<title>GATE XE 2024 | Question: 72</title>
<link>https://xe.gateoverflow.in/344/gate-xe-2024-question-72</link>
<description>&lt;p&gt;A beam of rectangular cross-section, as shown in the figure, is made of two perfectly bonded layers of different materials and equal thickness. The Young&#039;s moduli of the two materials are $E_{1}$ and $E_{2}$, where $E_{1}=2 E_{2}$. The beam is subjected to pure bending. If $t=1 \mathrm{~mm}$, the distance of the neutral plane from the top surface of the beam is __________&amp;nbsp;$\text{(in mm, rounded off to two decimal places)}$.&lt;/p&gt;

&lt;p style=&quot;text-align:center&quot;&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=6073080739177527292&quot; width=&quot;300&quot;&gt;&lt;/p&gt;

&lt;p&gt;&amp;nbsp;&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/344/gate-xe-2024-question-72</guid>
<pubDate>Sun, 21 Jul 2024 16:41:46 +0000</pubDate>
</item>
<item>
<title>GATE XE 2024 | Question: 73</title>
<link>https://xe.gateoverflow.in/343/gate-xe-2024-question-73</link>
<description>&lt;p&gt;A stepped beam is made of a material whose Young&#039;s modulus is $E$. The dimensions of the two stepped sections are such that the sectional moments of inertia, $I_{1}$ and $I_{2}$, are related as $I_{1}=8 I_{2}$. The beam is fixed at one end and a load of $F$ is applied at the free end as shown in the figure. Under this loading condition, if the strain energy of the stepped beam is written as $U=\beta \frac{F^{2} L^{3}}{E I_{1}}$, then the value of $\beta$ is ___________&amp;nbsp;$\text{(rounded off to two decimal places)}$.&lt;/p&gt;

&lt;p style=&quot;text-align:center&quot;&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=15220231618901864070&quot; width=&quot;400&quot;&gt;&lt;/p&gt;

&lt;p&gt;&amp;nbsp;&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/343/gate-xe-2024-question-73</guid>
<pubDate>Sun, 21 Jul 2024 16:41:45 +0000</pubDate>
</item>
<item>
<title>GATE XE 2024 | Question: 74</title>
<link>https://xe.gateoverflow.in/342/gate-xe-2024-question-74</link>
<description>&lt;p&gt;A cylindrical pressure vessel is constructed by bolting two symmetric halves of flanged semi-cylindrical shells. A cross-sectional view of the vessel is shown in the figure. The inner diameter of the vessel is $2$ m and the length is $10$ m. Each row comprises $100$ bolts along the length of the vessel. If the vessel is pressurized to a net pressure of $6 \times 10^{5} \mathrm{~N} / \mathrm{m}^{2}$, and assuming the end caps of the vessel do not take any load in the radial direction, then the load borne by each bolt is _________&amp;nbsp;$\text{(in kN, rounded off to onc decimal place)}$.&lt;/p&gt;

&lt;p style=&quot;text-align:center&quot;&gt;&lt;img alt=&quot;&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=14890843892188481895&quot; width=&quot;300&quot;&gt;&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/342/gate-xe-2024-question-74</guid>
<pubDate>Sun, 21 Jul 2024 16:41:44 +0000</pubDate>
</item>
<item>
<title>GATE XE 2023 | Question: 40</title>
<link>https://xe.gateoverflow.in/201/gate-xe-2023-question-40</link>
<description>&lt;img alt=&quot;GATE XE 2023 | Question-40&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=17482081357236931246&quot;&gt;&lt;p&gt;\begin{tabular}{c|c} &lt;br&gt;
Q. 50 &amp;amp; The tensile true stress $(\sigma)-$ true strain $(\epsilon)$ curve follows the Hollomon equation: \\&lt;br&gt;
$\qquad \sigma=500 \epsilon^{0.15} \mathrm{MPa}$ \\&lt;br&gt;
At the maximum load, the work-hardening rate $\left(\frac{d \sigma}{d \epsilon}\right)$ is (in $\left.\mathrm{MPa}\right):$ \\&lt;br&gt;
\hline&lt;br&gt;
\end{tabular}&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/201/gate-xe-2023-question-40</guid>
<pubDate>Wed, 14 Feb 2024 18:09:44 +0000</pubDate>
</item>
<item>
<title>GATE XE 2023 | Question: 58</title>
<link>https://xe.gateoverflow.in/183/gate-xe-2023-question-58</link>
<description>&lt;img alt=&quot;GATE XE 2023 | Question-58&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=5223355309938515820&quot;&gt;&lt;p&gt;\begin{tabular}{|c|c|}&lt;br&gt;
\hline Q. 68 &amp;amp; \begin{tabular}{l} &lt;br&gt;
Two equivalent descriptions of the state of stress at a point are shown in the \\&lt;br&gt;
figure. The normal stresses $\sigma_{1}$ and $\sigma_{2}$ as shown on the right must be, respectively,&lt;br&gt;
\end{tabular} \\&lt;br&gt;
\hline &amp;amp; \\&lt;br&gt;
\hline &lt;/p&gt;&lt;ol style=&quot;list-style-type:upper-alpha&quot;&gt;&lt;li&gt;  &amp;amp; $\tau_{\mathrm{o}}$ and $-\tau_{\mathrm{o}}$ \\&lt;br&gt;
\hline &lt;/li&gt;&lt;li&gt;  &amp;amp; $-\tau_{\mathrm{o}}$ and $\tau_{\mathrm{o}}$ \\&lt;br&gt;
\hline &lt;/li&gt; &lt;li&gt; &amp;amp; $\frac{\tau_{0}}{\sqrt{2}}$ and $-\frac{\tau_{0}}{\sqrt{2}}$ \\&lt;br&gt;
\hline &lt;/li&gt;  &lt;li&gt; &amp;amp; $-\frac{\tau_{0}}{\sqrt{2}}$ and $\frac{\tau_{0}}{\sqrt{2}}$ \\&lt;br&gt;
\hline&lt;br&gt;
\end{tabular}  &lt;/li&gt;&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/183/gate-xe-2023-question-58</guid>
<pubDate>Wed, 14 Feb 2024 18:09:27 +0000</pubDate>
</item>
<item>
<title>GATE XE 2023 | Question: 59</title>
<link>https://xe.gateoverflow.in/182/gate-xe-2023-question-59</link>
<description>&lt;img alt=&quot;GATE XE 2023 | Question-59&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=6717061832051747301&quot;&gt;&lt;p&gt;\begin{tabular}{l|l} &lt;br&gt;
Q.69 &amp;amp; The state of strain at a point in a machine component is given as \\&lt;br&gt;
$\varepsilon_{x x}=2.5 \times 10^{-4}, \varepsilon_{y y}=2.0 \times 10^{-4}, \varepsilon_{z z}=-1.5 \times 10^{-4}, \varepsilon_{x y}=2.5 \times 10^{-4}$, \\&lt;br&gt;
$\varepsilon_{y z}=-0.5 \times 10^{-4}, \varepsilon_{z x}=-1.0 \times 10^{-4}$. The volumetric strain at this point is \\&lt;br&gt;
&lt;/p&gt;&lt;ol style=&quot;list-style-type:upper-alpha&quot;&gt;&lt;li&gt;  &amp;amp; $4 \times 10^{-4}$ \\&lt;br&gt;
\hline &lt;/li&gt;&lt;li&gt;  &amp;amp; $3 \times 10^{-4}$ \\&lt;br&gt; &lt;/li&gt; &lt;li&gt; &amp;amp; $-5 \times 10^{-4}$ \\&lt;br&gt; &lt;/li&gt;  &lt;li&gt; &amp;amp; $-3 \times 10^{-4}$&lt;br&gt;
\end{tabular}  &lt;/li&gt;&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/182/gate-xe-2023-question-59</guid>
<pubDate>Wed, 14 Feb 2024 18:09:26 +0000</pubDate>
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<item>
<title>GATE XE 2023 | Question: 60</title>
<link>https://xe.gateoverflow.in/181/gate-xe-2023-question-60</link>
<description>&lt;img alt=&quot;GATE XE 2023 | Question-60&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=17570264024523010078&quot;&gt;&lt;p&gt;\begin{tabular}{|l|l|}&lt;br&gt;
\hline Q.70 &amp;amp; A thin walled, closed cylindrical vessel of inside diameter $d$ and wall thickness $t$ \\&lt;br&gt;
contains a fluid under pressure $p$. The figure below shows a part of the cylindrical \\&lt;br&gt;
vessel; end caps are not shown. Consider the small element shown with sides \\&lt;br&gt;
parallel and perpendicular to the axis of the cylinder. The stresses $\sigma_{1}$ and $\sigma_{2}$ are \\&lt;br&gt;
\hline &lt;/p&gt;&lt;ol style=&quot;list-style-type:upper-alpha&quot;&gt;&lt;li&gt;  &amp;amp; $\sigma_{1}=\frac{p d}{2 t} ; \sigma_{2}=\frac{p d}{4 t}$ \\&lt;br&gt; &lt;/li&gt;&lt;li&gt;  &amp;amp; $\sigma_{1}=\frac{p d}{t} ; \sigma_{2}=\frac{p d}{2 t}$ \\&lt;br&gt; &lt;/li&gt; &lt;li&gt; &amp;amp; $\sigma_{1}=\frac{p d}{4 t} ; \sigma_{2}=\frac{p d}{2 t}$ \\&lt;br&gt; &lt;/li&gt;  &lt;li&gt; &amp;amp; $\sigma_{1}=\frac{p d}{2 t} ; \sigma_{2}=0$ \\&lt;br&gt;
\hline&lt;br&gt;
\end{tabular}  &lt;/li&gt;&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/181/gate-xe-2023-question-60</guid>
<pubDate>Wed, 14 Feb 2024 18:09:25 +0000</pubDate>
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<item>
<title>GATE XE 2023 | Question: 64</title>
<link>https://xe.gateoverflow.in/177/gate-xe-2023-question-64</link>
<description>&lt;img alt=&quot;GATE XE 2023 | Question-64&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=6039196388985429049&quot;&gt;&lt;p&gt;\[&lt;br&gt;
\text { Q. } 74&lt;br&gt;
\]&lt;br&gt;
&lt;br&gt;
For a plane stress problem, the principal stresses are $100 \mathrm{MPa}$ and $50 \mathrm{MPa}$. The magnitude of maximum shear stress (in $\mathrm{MPa}$ ) in the material is (rounded off to one decimal place).&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/177/gate-xe-2023-question-64</guid>
<pubDate>Wed, 14 Feb 2024 18:09:21 +0000</pubDate>
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<item>
<title>GATE XE 2023 | Question: 66</title>
<link>https://xe.gateoverflow.in/175/gate-xe-2023-question-66</link>
<description>&lt;img alt=&quot;GATE XE 2023 | Question-66&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=1637288877561295033&quot;&gt;&lt;p&gt;\begin{tabular}{|l|l|}&lt;br&gt;
\hline Q.76 &amp;amp; A cylinder made of rubber (length $=L$ and diameter $=d)$ is inserted in a rigid \\&lt;br&gt;
container as shown in the figure. The rubber cylinder fits snugly in the rigid \\&lt;br&gt;
container. There is no wall friction. The modulus of elasticity of the rubber is $E$ \\&lt;br&gt;
and its Poisson&#039;s ratio is $v$. The cylinder is subjected to a small uniform pressure $p$ \\&lt;br&gt;
as shown in the figure. The resulting axial strain $\left(\varepsilon_{z z}\right)$ is \\&lt;br&gt;
\hline &lt;/p&gt;&lt;ol style=&quot;list-style-type:upper-alpha&quot;&gt;&lt;li&gt;  \\&lt;br&gt; &lt;/li&gt;&lt;li&gt;  &amp;amp; $-\frac{p}{E}$ \\&lt;br&gt;
\hline &lt;/li&gt; &lt;li&gt; \\&lt;br&gt; &lt;/li&gt;  &lt;li&gt; \\&lt;br&gt;
$-\frac{p}{E}\left[\frac{(1+v)(1-2 v)}{(1-v)}\right]$ \\&lt;br&gt;
\hline&lt;br&gt;
\end{tabular}  &lt;/li&gt;&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/175/gate-xe-2023-question-66</guid>
<pubDate>Wed, 14 Feb 2024 18:09:19 +0000</pubDate>
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<item>
<title>GATE XE 2023 | Question: 67</title>
<link>https://xe.gateoverflow.in/174/gate-xe-2023-question-67</link>
<description>&lt;img alt=&quot;GATE XE 2023 | Question-67&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=4314310245349606038&quot;&gt;&lt;p&gt;\begin{tabular}{|c|}&lt;br&gt;
\hline \begin{tabular}{l} &lt;br&gt;
The state of stress at the critical location in a structure is $\sigma_{x x}=420 \mathrm{MPa}$, \\&lt;br&gt;
$\sigma_{y y}=100 \mathrm{MPa}, \sigma_{z z}=\sigma_{x y}=\sigma_{y z}=\sigma_{z x}=0$. The yield stress of the material in \\&lt;br&gt;
uniaxial tension is $400 \mathrm{MPa}$. Select the correct statement among the following.&lt;br&gt;
\end{tabular} \\&lt;br&gt;
\hline \begin{tabular}{l} &lt;br&gt;
The structure is safe by both Tresca (maximum shear stress) theory and von-Mises \\&lt;br&gt;
(distortion energy) theory.&lt;br&gt;
\end{tabular} \\&lt;br&gt;
\hline \begin{tabular}{l} &lt;br&gt;
The structure is safe by Tresca (maximum shear stress) theory and unsafe by \\&lt;br&gt;
von-Mises (distortion energy) theory.&lt;br&gt;
\end{tabular} \\&lt;br&gt;
\hline \begin{tabular}{l} &lt;br&gt;
The structure is unsafe by Tresca (maximum shear stress) theory and safe by \\&lt;br&gt;
von-Mises (distortion energy) theory.&lt;br&gt;
\end{tabular} \\&lt;br&gt;
\hline \begin{tabular}{l} &lt;br&gt;
The structure is unsafe by both Tresca (maximum shear stress) theory and \\&lt;br&gt;
von-Mises (distortion energy) theory.&lt;br&gt;
\end{tabular} \\&lt;br&gt;
\hline&lt;br&gt;
\end{tabular}&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/174/gate-xe-2023-question-67</guid>
<pubDate>Wed, 14 Feb 2024 18:09:17 +0000</pubDate>
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<item>
<title>GATE XE 2023 | Question: 68</title>
<link>https://xe.gateoverflow.in/173/gate-xe-2023-question-68</link>
<description>&lt;img alt=&quot;GATE XE 2023 | Question-68&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=7708370515307409239&quot;&gt;&lt;p&gt;Q. 78&lt;br&gt;
The figure shows a column of rectangular cross section $100 \mathrm{~mm} \times 80 \mathrm{~mm}$. It&lt;br&gt;
carries a load of $60 \mathrm{kN}$ at a point $30 \mathrm{~mm}$ from the edge $P Q$. The values of stress&lt;br&gt;
component $\sigma_{z z}$ on surfaces $P Q Q^{\prime} P^{\prime}$ and $S R R^{\prime} S^{\prime}$, at points far away from both&lt;br&gt;
ends of the column, are respectively&lt;br&gt;
(C)&lt;br&gt;
(D)&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/173/gate-xe-2023-question-68</guid>
<pubDate>Wed, 14 Feb 2024 18:09:16 +0000</pubDate>
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<item>
<title>GATE XE 2023 | Question: 69</title>
<link>https://xe.gateoverflow.in/172/gate-xe-2023-question-69</link>
<description>&lt;img alt=&quot;GATE XE 2023 | Question-69&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=11520175926480927454&quot;&gt;&lt;p&gt;\begin{tabular}{|l|l} &lt;br&gt;
Q.79 &amp;amp; Consider an electric pole with dimensions as shown in the figure. Let the end $R$ be \\&lt;br&gt;
subjected to a vertical force $F$. The flexural rigidity of both vertical and horizontal \\&lt;br&gt;
bars is $E I$. Neglect the axial deflection of the vertical bar, and all effects of \\&lt;br&gt;
self-weight. The vertical deflection at end $R$ is \\&lt;br&gt;
(A) &amp;amp; $\frac{7 F L^{3}}{3 E I}$ \\&lt;br&gt;
(B) &amp;amp; $\frac{10 F L^{3}}{3 E I}$ \\&lt;br&gt;
(C) &amp;amp; $\frac{5 F L^{3}}{3 E I}$ \\&lt;br&gt;
\hline&lt;br&gt;
\end{tabular}&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/172/gate-xe-2023-question-69</guid>
<pubDate>Wed, 14 Feb 2024 18:09:15 +0000</pubDate>
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<item>
<title>GATE XE 2023 | Question: 70</title>
<link>https://xe.gateoverflow.in/171/gate-xe-2023-question-70</link>
<description>&lt;img alt=&quot;GATE XE 2023 | Question-70&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=11863654685086363762&quot;&gt;&lt;p&gt;Q.80 A uniform cantilever beam has flexural rigidity $E I$ and length $L$. It is subjected to&lt;br&gt;
a concentrated force $F$ and moment $M=2 F L$ at the free end as shown. The&lt;br&gt;
deflection $(\delta)$ at the free end is&lt;br&gt;
&lt;/p&gt;&lt;ol style=&quot;list-style-type:upper-alpha&quot;&gt;&lt;li&gt;  $\frac{11 F L^{3}}{12 E I}$&lt;br&gt; &lt;/li&gt;&lt;li&gt;  $\frac{8 F L^{3}}{9 E I}$&lt;br&gt; &lt;/li&gt; &lt;li&gt; $\frac{4 F L^{3}}{3 E I}$&lt;br&gt; &lt;/li&gt;  &lt;li&gt; $\frac{7 F L^{3}}{6 E I}$  &lt;/li&gt;&lt;/ol&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/171/gate-xe-2023-question-70</guid>
<pubDate>Wed, 14 Feb 2024 18:09:14 +0000</pubDate>
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<item>
<title>GATE XE 2023 | Question: 74</title>
<link>https://xe.gateoverflow.in/167/gate-xe-2023-question-74</link>
<description>&lt;img alt=&quot;GATE XE 2023 | Question-74&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=15787176697347530103&quot;&gt;&lt;p&gt;Q. 84&lt;br&gt;
A thin steel plate is loaded in the $x$-y plane as shown in the figure. Take the&lt;br&gt;
Poisson&#039;s ratio of steel to be 0.3 and the modulus of elasticity of steel to be 200&lt;br&gt;
$\mathrm{GPa}$. The strain along the $z$-direction is $\varepsilon_{\mathrm{zz}}=-3 \times 10^{-4}$. The value of $\sigma_{y y}$ (in&lt;br&gt;
$\mathrm{MPa}$ ) is___unded off to one decimal place).&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/167/gate-xe-2023-question-74</guid>
<pubDate>Wed, 14 Feb 2024 18:09:11 +0000</pubDate>
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<item>
<title>GATE XE 2023 | Question: 76</title>
<link>https://xe.gateoverflow.in/165/gate-xe-2023-question-76</link>
<description>&lt;img alt=&quot;GATE XE 2023 | Question-76&quot; src=&quot;https://xe.gateoverflow.in/?qa=blob&amp;amp;qa_blobid=12431339013360791444&quot;&gt;&lt;p&gt;Q. 86 A slender uniform elastic rod of length $1 \mathrm{~m}$ and of solid circular cross-section of diameter $50 \mathrm{~mm}$ is originally straight. It is then loaded by equal and opposite end moments as indicated in the figure. The resulting lateral displacement of the mid-point of the rod is $10 \mathrm{~mm}$ (displacements are exaggerated in the figure). The maximum longitudinal strain in the rod is $p \times 10^{-3}$, where $p$ is (rounded off to one decimal place).&lt;/p&gt;</description>
<category>Mechanics of deformable bodies</category>
<guid isPermaLink="true">https://xe.gateoverflow.in/165/gate-xe-2023-question-76</guid>
<pubDate>Wed, 14 Feb 2024 18:09:09 +0000</pubDate>
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