Strength of Materials
Pure Bending
Marks 1Marks 2
Stresses In Beams
Marks 1Marks 2
Simple Stress and Strain
Marks 1Marks 2
Complex Stresses
Marks 1Marks 2
Moment of Inertia
Marks 1Marks 2
Deflection of Beams
Marks 1Marks 2
Shear Force and Bending Moment
Marks 1Marks 2
Thin Cylinders
Marks 1Marks 2
Columns and Struts
Marks 1Marks 2
Strain Energy Method
Marks 1Marks 2
1
GATE ME 2022 Set 2
MCQ (Single Correct Answer)
+1
-0.33
A structural member under loading has a uniform state of plane stress which in usual notations is given by Ïƒ= 3P, Ïƒy = -2P and Ï„xy = √2 P, where P > 0. The yield strength of the material is 350 MPa. If the member is designed using the maximum distortion energy theory, then the value of P at which yielding starts (according to the maximum distortion energy theory) is
A
70 MPa
B
90 MPa
C
120 MPa
D
75 MPa
2
GATE ME 2022 Set 1
MCQ (More than One Correct Answer)
+1
-0
Assuming the material considered in each statement is homogeneous, isotropic, linear elastic, and the deformations are in the elastic range, which one or more of the following statement(s) is/are TRUE?
A
A body subjected to hydrostatic pressure has no shear stress
B
If a long solid steel rod is subjected to tensile load, then its volume increases
C
Maximum shear stress theory is suitable for failure analysis of brittle materials
D
If a portion of a beam has zero shear force, then the corresponding portion of the elastic curve of the beam is always straight.
3
GATE ME 2017 Set 2
Numerical
+1
-0
The state of stress at a point is $${\sigma _x} = {\sigma _y} = {\sigma _z} = {\tau _{xz}} = {\tau _{zx}} = {\tau _{yz}} = {\tau _{zy}} = 0$$ and $${\tau _{xy}} = {\tau _{yx}} = 50$$MPa. The maximum normal stress (in MPa) at the point is _________.
Your input ____
4
GATE ME 2016 Set 3
MCQ (Single Correct Answer)
+1
-0.3
The state of stress at a point on an element is shown in figure (a). The same state of stress is shownin another coordinate system in figure (b). GATE ME 2016 Set 3 Strength of Materials - Complex Stresses Question 23 English

The components $$\left( {{\tau _{xx,}}{\tau _{yy,}}{\tau _{xy}}} \right)$$ are given by

A
$$\left( {P/\sqrt {\mathop {\lim }\limits_{x \to \infty } 2} , - P/\sqrt 2 ,0} \right)$$
B
$$\left( {0,0,P} \right)$$
C
$$\left( {P, - P, - P/\sqrt 2 } \right)$$
D
$$\left( {0,0,P/\sqrt 2 } \right)$$
GATE ME Subjects
Engineering Mechanics
Machine Design
Strength of Materials
Heat Transfer
Production Engineering
Industrial Engineering
Turbo Machinery
Theory of Machines
Engineering Mathematics
Fluid Mechanics
Thermodynamics
General Aptitude