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ENGINEERING MECHANICS & STRENGTH OF MATERIALS – MCQ THINKING GUIDE
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🧠 Strategy:
First understand the physical principle → Then eliminate wrong options → Then confirm formula.
Q1) In a simply supported beam of length L, a UDL of w kN/m acts on the entire span.
The maximum bending moment will be:
a) wL²/8
b) wL³/8
c) wL²/4
d) wL³/4
UDL over full span → Maximum BM at mid-span.
Standard formula:
✅ (a) wL² / 8
🧠 Simply supported + UDL → “L² over 8”
Q2) If two forces are acting on a particle and the particle is in stable equilibrium, then the forces are:
a) Equal to each other
b) Equal but opposite in direction
c) Unequal but same direction
d) None of the above
For equilibrium under two forces:
Equal magnitude + Opposite direction + Same line of action.
✅ (b) Equal but opposite in direction
🧠 Only two forces? → They must cancel perfectly.
Q3) The example of statically indeterminate structures are:
a) Continuous beam
b) Cantilever beam
c) Over-hanging beam
d) Both cantilever and fixed beam
Indeterminate → More unknown reactions than equilibrium equations.
Continuous beam has extra supports.
✅ (a) Continuous beam
🧠 Extra supports = Extra unknowns = Indeterminate
Q4) A redundant truss satisfies:
a) m = 2j − 3
b) m < 2j + 3
c) m > 2j − 3
d) m > 2j + 3
Perfect truss: m = 2j − 3
More members → Redundant
✅ (c) m > 2j − 3
🧠 “More members than needed” = Redundant
Q5) Property of a material to withstand sudden shock is:
a) Hardness
b) Ductility
c) Toughness
d) Elasticity
Shock → Energy absorption → Toughness.
✅ (c) Toughness
🧠 Impact resistance = Toughness
Q6) Stress generated by a dynamic loading is approximately ____ times the stress developed by gradually applying the same load.
Suddenly applied load causes double stress.
✅ 2 times
🧠 Sudden load → Double stress
Q7) The ratio between volumetric stress and volumetric strain is:
a) Young's modulus
b) Modulus of elasticity
c) Rigidity modulus
d) Bulk modulus
Volume change relation → Bulk modulus.
✅ (d) Bulk modulus
🧠 Volume → Bulk modulus
Q8) In a cantilever beam, maximum bending moment is induced at:
a) Free end
b) Fixed end
c) Mid span
d) None of the above
Cantilever fixed at one end → Maximum BM at fixed support.
✅ (b) At the fixed end
🧠 Cantilever cries at fixed end.
Q9) Forces which meet at a point are called:
a) Collinear forces
b) Concurrent forces
c) Coplanar forces
d) Parallel forces
Concurrent → Intersect at one point.
✅ (b) Concurrent forces
🧠 Meet at one point → Concurrent
Q10) The coefficient of friction depends upon:
a) Nature of the surface
b) Shape of the surface
c) Area of contact
d) Weight of body
Independent of area & weight.
Depends on surface nature.
✅ (a) Nature of the surface
🧠 Roughness matters. Area doesn’t.
Q11) Variation of shear force due to triangular load on simply supported beam is:
a) Uniform
b) Linear
c) Parabolic
d) Cubic
Load is linear → Shear is integral → Parabolic.
✅ (c) Parabolic
🧠 Load linear → Shear parabolic → BM cubic
Q12) A body is on the point of sliding down a 30° inclined plane.
Coefficient of friction is:
a) \( (\frac{1}{3})^{\frac{1}{2}} \)
b) √3
c) 1
d) 0
At limiting equilibrium:
μ = tanθ
μ = tan30° = 1/√3
✅ (a) \( (\frac{1}{3})^{\frac{1}{2}} \)
🧠 On verge of sliding → μ = tanθ
FINAL NEURAL COMPRESSION TABLE
Concept
Quick Memory Code
UDL BM
wL²/8
Sudden Load
2 × Stress
Perfect Truss
m = 2j − 3
Friction Limit
μ = tanθ
🧠 When formula connects with physical meaning,
MCQs become recognition — not rote memory.
ENGINEERING MECHANICS & SOM – MCQ PRACTICE SET 2
🧠 Think Like an Engineer:
Every MCQ is testing one core law:
Equilibrium • Compatibility • Constitutive relation • Load–Shear–Moment relation
Q1) For a simply supported beam with a central point load W, the maximum bending moment is:
a) WL/2
b) WL/4
c) WL/8
d) WL²/8
Central point load → Maximum BM at mid-span.
Standard formula:
✅ (b) WL / 4
🧠 Point load center → “L over 4”
Q2) A body is said to be in equilibrium when:
a) Only ∑F = 0
b) Only ∑M = 0
c) ∑F = 0 and ∑M = 0
d) Acceleration is constant
Static equilibrium requires:
Sum of forces = 0
Sum of moments = 0
✅ (c) ∑F = 0 and ∑M = 0
🧠 No translation + No rotation = Equilibrium
Q3) A cantilever beam carrying a point load at free end has maximum shear force at:
a) Free end
b) Fixed end
c) Mid span
d) Zero everywhere
Shear force is maximum at fixed support.
✅ (b) Fixed end
🧠 Cantilever suffers at the fixed end.
Q4) For a perfect frame (plane truss), the relation between members (m) and joints (j) is:
a) m = 2j + 3
b) m = 2j − 3
c) m = j − 3
d) m = 3j − 2
Condition of perfect truss:
✅ (b) m = 2j − 3
🧠 Perfect truss = 2j minus 3
Q5) The ratio of lateral strain to longitudinal strain is called:
a) Young’s modulus
b) Bulk modulus
c) Poisson’s ratio
d) Rigidity modulus
Lateral contraction / Axial extension
✅ (c) Poisson’s ratio
🧠 Stretch long → Shrink sideways → Poisson
Q6) The bending moment at the free end of a cantilever beam is:
a) Maximum
b) Minimum
c) Zero
d) Infinite
Free end cannot resist moment.
✅ (c) Zero
🧠 Free end = Free from moment.
Q7) If load intensity is constant, the shear force diagram will be:
a) Linear
b) Parabolic
c) Cubic
d) Constant
UDL is constant → Shear force varies linearly.
✅ (a) Linear
🧠 Load constant → Shear straight line
Q8) The strain energy stored in a body depends upon:
a) Load only
b) Stress only
c) Stress and strain
d) Volume only
Strain energy = (1/2) × stress × strain × volume
✅ (c) Stress and strain
🧠 Energy lives where stress meets strain.
Q9) The angle of friction is defined as:
a) Angle between normal reaction and resultant reaction
b) Angle between weight and plane
c) Angle between friction and plane
d) Angle of slope
Angle between resultant reaction and normal reaction.
✅ (a)
🧠 Resultant reaction tilts by angle of friction.
Q10) A beam subjected to pure bending experiences:
a) Shear stress only
b) Normal stress only
c) Both shear and normal stress
d) No stress
Pure bending → No shear force → Only bending stress.
✅ (b) Normal stress only
🧠 Pure bending → Pure normal stress.
Q11) The modulus of rigidity relates:
a) Normal stress & longitudinal strain
b) Shear stress & shear strain
c) Volumetric stress & volumetric strain
d) Bending stress & curvature
Rigidity modulus (G) → Shear relationship.
✅ (b) Shear stress & shear strain
🧠 Rigidity = Resistance to shear.
Q12) A simply supported beam with no external load will have:
a) Zero shear and zero bending moment
b) Maximum shear
c) Maximum bending moment
d) Uniform moment
No load → No reactions → No internal forces.
✅ (a) Zero shear and zero bending moment
🧠 No load → No stress → Peaceful beam.
FINAL PATTERN MAP
Topic
Core Trigger
Simply Supported (Point Load)
WL/4
Perfect Truss
m = 2j − 3
Friction Limit
μ = tanθ
Pure Bending
No shear stress
🧠 When you see the question,
ask: “Which law is hiding here?”
That is how toppers think.
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