Strength of Materials – 100 One-Liner MCQs
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Stress is defined as
A) Load/Area ✔️
B) Area/Load
C) Load×Area
D) Area²/Load
Ans: A -
Strain is the ratio of
A) Change in length to original length ✔️
B) Load to area
C) Stress to strain
D) Force to length
Ans: A -
Unit of stress is
A) N/m² ✔️
B) N
C) m²
D) kg
Ans: A -
Hooke’s law is valid up to
A) Elastic limit ✔️
B) Yield point
C) Breaking point
D) Ultimate stress
Ans: A -
Young’s modulus is ratio of
A) Stress/Strain ✔️
B) Strain/Stress
C) Load/Area
D) Force/Length
Ans: A -
Bulk modulus relates to
A) Volumetric strain ✔️
B) Linear strain
C) Shear strain
D) Thermal strain
Ans: A -
Modulus of rigidity relates to
A) Shear stress & shear strain ✔️
B) Normal stress & strain
C) Volumetric stress
D) Bending stress
Ans: A -
Poisson’s ratio is
A) Lateral strain/Longitudinal strain ✔️
B) Longitudinal/Lateral
C) Stress/Strain
D) Load/Area
Ans: A -
Value of Poisson’s ratio lies between
A) 0 to 0.5 ✔️
B) 0.5 to 1
C) 1 to 2
D) −1 to 1
Ans: A -
Ultimate stress is
A) Maximum stress material can withstand ✔️
B) Elastic stress
C) Yield stress
D) Breaking stress
Ans: A
-
Factor of safety =
A) Ultimate stress / Working stress ✔️
B) Working/Ultimate
C) Yield/Working
D) Breaking/Area
Ans: A -
Brittle materials fail mainly by
A) Tensile stress ✔️
B) Compressive stress
C) Shear stress
D) Torsion
Ans: A -
Ductile materials show
A) Large plastic deformation ✔️
B) No deformation
C) Sudden failure
D) No necking
Ans: A -
Resilience is
A) Energy absorbed in elastic limit ✔️
B) Total energy absorbed
C) Energy at fracture
D) Plastic energy
Ans: A -
Proof resilience is
A) Maximum elastic strain energy ✔️
B) Total strain energy
C) Plastic energy
D) Impact energy
Ans: A -
Toughness is
A) Energy absorbed before fracture ✔️
B) Energy in elastic range
C) Resistance to indentation
D) Resistance to corrosion
Ans: A -
Hardness means
A) Resistance to scratching ✔️
B) Resistance to bending
C) Resistance to fatigue
D) Resistance to heat
Ans: A -
Creep occurs mainly due to
A) Constant load at high temperature ✔️
B) Variable load
C) Impact load
D) Sudden load
Ans: A -
Fatigue is failure due to
A) Repeated loading ✔️
B) Static loading
C) Impact loading
D) Thermal loading
Ans: A -
Endurance limit is
A) Stress below which failure never occurs ✔️
B) Breaking stress
C) Yield stress
D) Ultimate stress
Ans: A
-
Axial deformation of a bar depends on
A) Load, length, area, E ✔️
B) Only load
C) Only length
D) Only area
Ans: A -
Stress in bar under axial load =
A) P/A ✔️
B) P×A
C) A/P
D) P²/A
Ans: A -
Thermal stress develops when
A) Expansion is restrained ✔️
B) Free expansion occurs
C) Cooling only
D) Heating only
Ans: A -
Thermal strain =
A) αΔT ✔️
B) ΔT/α
C) α/ΔT
D) αΔT²
Ans: A -
Complementary shear stresses are
A) Equal in magnitude ✔️
B) Unequal
C) Opposite in direction
D) Zero
Ans: A -
Principal stresses occur on planes where
A) Shear stress is zero ✔️
B) Normal stress is zero
C) Bending is zero
D) Torsion is zero
Ans: A -
Maximum shear stress occurs at
A) 45° to principal plane ✔️
B) 0°
C) 90°
D) 60°
Ans: A -
Mohr’s circle is used to find
A) Principal stresses ✔️
B) Bending moment
C) Shear force
D) Deflection
Ans: A -
State of pure shear has
A) Zero normal stress ✔️
B) Zero shear stress
C) Equal normal stresses
D) Only bending stress
Ans: A -
Maximum principal stress equals
A) Center + radius of Mohr’s circle ✔️
B) Center − radius
C) Radius only
D) Diameter
Ans: A
-
Neutral axis in bending passes through
A) Centroid ✔️
B) Top fiber
C) Bottom fiber
D) Shear center
Ans: A -
Bending stress formula is
A) σ = My/I ✔️
B) σ = My
C) σ = M/I
D) σ = Iy/M
Ans: A -
Maximum bending stress occurs at
A) Farthest fiber from N.A. ✔️
B) Neutral axis
C) Centroid
D) Shear center
Ans: A -
Section modulus Z =
A) I/ymax ✔️
B) I×ymax
C) y/I
D) A/y
Ans: A -
Stronger beam section is one with
A) Larger section modulus ✔️
B) Larger area
C) Larger length
D) Larger weight
Ans: A -
In cantilever beam, maximum BM occurs at
A) Fixed end ✔️
B) Free end
C) Mid span
D) Quarter span
Ans: A -
In simply supported beam with UDL, max BM at
A) Mid span ✔️
B) Supports
C) Quarter span
D) One-third span
Ans: A -
Shear force is maximum at
A) Supports ✔️
B) Mid span
C) Neutral axis
D) Centroid
Ans: A -
Point of contraflexure is where
A) BM changes sign ✔️
B) SF is zero
C) Deflection is max
D) Stress is zero
Ans: A -
Deflection of beam depends on
A) EI ✔️
B) Only load
C) Only length
D) Only area
Ans: A
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Torsion equation is
A) T/J = τ/R = Gθ/L ✔️
B) T/J = σ/y
C) M/I = σ/y
D) P/A
Ans: A -
Polar moment of inertia is denoted by
A) J ✔️
B) I
C) Z
D) A
Ans: A -
Torsional rigidity =
A) GJ ✔️
B) EI
C) EA
D) E/G
Ans: A -
Shear stress in shaft varies
A) Linearly with radius ✔️
B) Constant
C) Parabolic
D) Random
Ans: A -
Maximum shear stress in solid shaft occurs at
A) Outer surface ✔️
B) Center
C) Mid radius
D) Neutral axis
Ans: A -
Hollow shaft is stronger than solid shaft of same weight because
A) Material is away from center ✔️
B) More area
C) More mass
D) Less length
Ans: A -
Angle of twist depends on
A) T, L, G, J ✔️
B) Only torque
C) Only length
D) Only diameter
Ans: A -
Power transmitted by shaft =
A) 2πNT/60 ✔️
B) NT
C) T/N
D) N/T
Ans: A -
Maximum shear stress theory is also called
A) Tresca theory ✔️
B) Rankine theory
C) Guest theory
D) St. Venant theory
Ans: A -
Maximum principal stress theory is
A) Rankine theory ✔️
B) Tresca theory
C) Von Mises theory
D) Guest theory
Ans: A
-
Maximum shear strain energy theory is
A) Von Mises theory ✔️
B) Rankine theory
C) Tresca theory
D) Coulomb theory
Ans: A -
Column fails by
A) Buckling ✔️
B) Bending
C) Torsion
D) Shear
Ans: A -
Slenderness ratio =
A) Effective length / Radius of gyration ✔️
B) Length / Area
C) Area / Length
D) I/A
Ans: A -
Euler’s formula is applicable for
A) Long columns ✔️
B) Short columns
C) Intermediate columns
D) All columns
Ans: A -
Critical load of column is
A) Buckling load ✔️
B) Breaking load
C) Yield load
D) Impact load
Ans: A -
End condition factor affects
A) Effective length ✔️
B) Area
C) Stress
D) Strain
Ans: A -
Rankine formula is used for
A) All columns ✔️
B) Only long
C) Only short
D) Only intermediate
Ans: A -
Maximum deflection of simply supported beam with UDL is at
A) Mid span ✔️
B) Supports
C) One-third span
D) Quarter span
Ans: A -
Strain energy stored in a body is due to
A) Deformation ✔️
B) Temperature
C) Mass
D) Gravity
Ans: A -
Impact factor increases when
A) Height of fall increases ✔️
B) Load decreases
C) Area increases
D) Length decreases
Ans: A
-
Stress concentration occurs due to
A) Sudden change in cross-section ✔️
B) Uniform section
C) Long length
D) High temperature
Ans: A -
Stress concentration factor =
A) Max stress / Nominal stress ✔️
B) Nominal/Max
C) Load/Area
D) Stress/Strain
Ans: A -
Fillets are provided to
A) Reduce stress concentration ✔️
B) Increase stress
C) Reduce weight
D) Increase stiffness
Ans: A -
Strain rosette is used to measure
A) Strains in different directions ✔️
B) Loads
C) Deflection
D) Temperature
Ans: A -
Plane stress condition occurs in
A) Thin plates ✔️
B) Thick blocks
C) Shafts
D) Columns
Ans: A -
Plane strain condition occurs in
A) Long dams ✔️
B) Thin plates
C) Shafts
D) Beams
Ans: A -
Elastic constants relation is
A) E = 2G(1+μ) ✔️
B) E = G/μ
C) E = μ/G
D) E = G(1−μ)
Ans: A -
Bulk modulus K relates as
A) E = 3K(1−2μ) ✔️
B) E = K(1+μ)
C) E = K/μ
D) E = K²
Ans: A -
Neutral layer in bending has
A) Zero stress ✔️
B) Max stress
C) Max strain
D) Max shear
Ans: A -
Shear stress distribution in rectangular beam is
A) Parabolic ✔️
B) Linear
C) Constant
D) Triangular
Ans: A
-
Max shear stress in rectangular beam occurs at
A) Neutral axis ✔️
B) Top fiber
C) Bottom fiber
D) Corners
Ans: A -
In circular shaft, shear stress distribution is
A) Linear ✔️
B) Parabolic
C) Constant
D) Sinusoidal
Ans: A -
Bending moment is zero at
A) Free end of cantilever ✔️
B) Fixed end
C) Mid span
D) Support of fixed beam
Ans: A -
Shear force diagram slope gives
A) Load intensity ✔️
B) Bending moment
C) Deflection
D) Stress
Ans: A -
Bending moment diagram slope gives
A) Shear force ✔️
B) Load
C) Stress
D) Deflection
Ans: A -
Cast iron is a
A) Brittle material ✔️
B) Ductile material
C) Elastic material
D) Plastic material
Ans: A -
Steel is generally
A) Ductile ✔️
B) Brittle
C) Non-elastic
D) Fragile
Ans: A -
Proof stress is used for
A) Materials without clear yield point ✔️
B) Brittle materials
C) Plastics only
D) Rubber
Ans: A -
Hooke’s law is
A) Stress ∝ Strain ✔️
B) Stress ∝ Load
C) Stress ∝ Area
D) Stress ∝ Length
Ans: A -
Modulus of elasticity indicates
A) Stiffness ✔️
B) Strength
C) Toughness
D) Hardness
Ans: A
-
Strain energy per unit volume is
A) Proof resilience ✔️
B) Toughness
C) Hardness
D) Ductility
Ans: A -
Maximum bending stress is proportional to
A) Bending moment ✔️
B) Shear force
C) Deflection
D) Area
Ans: A -
Buckling is
A) Sudden lateral deflection ✔️
B) Tensile failure
C) Shear failure
D) Torsional failure
Ans: A -
Euler’s critical load ∝
A) 1/L² ✔️
B) L
C) L²
D) L³
Ans: A -
Stress in a bar due to temperature rise is zero if
A) Bar is free to expand ✔️
B) Bar is fixed
C) Bar is cooled
D) Bar is loaded
Ans: A -
Elastic limit is
A) Max stress without permanent deformation ✔️
B) Yield stress
C) Breaking stress
D) Ultimate stress
Ans: A -
Plastic deformation starts after
A) Yield point ✔️
B) Elastic limit
C) Proportional limit
D) Breaking point
Ans: A -
Working stress is
A) Ultimate stress / FOS ✔️
B) Yield stress
C) Breaking stress
D) Proof stress
Ans: A -
Complementary shear stresses act on
A) Mutually perpendicular planes ✔️
B) Parallel planes
C) Inclined planes
D) Random planes
Ans: A -
Neutral axis shifts when
A) Section is unsymmetrical ✔️
B) Section is symmetrical
C) Load is zero
D) Moment is zero
Ans: A
-
In pure bending, shear force is
A) Zero ✔️
B) Maximum
C) Constant
D) Negative
Ans: A -
Shear center is point where
A) Load causes no twisting ✔️
B) Load causes bending only
C) Load causes shear only
D) Load causes tension only
Ans: A -
Cast iron is best in
A) Compression ✔️
B) Tension
C) Shear
D) Torsion
Ans: A -
Deflection increases if
A) Span increases ✔️
B) EI increases
C) Depth increases
D) Width increases
Ans: A -
Strain is
A) Dimensionless ✔️
B) In N
C) In m
D) In kg
Ans: A -
Stress-strain curve of ductile material shows
A) Yield plateau ✔️
B) Sudden break
C) No plastic zone
D) No elastic zone
Ans: A -
Toughness is area under
A) Entire stress-strain curve ✔️
B) Elastic portion only
C) Plastic portion only
D) Yield region only
Ans: A -
Resilience is area under
A) Elastic portion of curve ✔️
B) Plastic portion
C) Entire curve
D) Yield portion
Ans: A -
Column with both ends fixed has effective length
A) L/2 ✔️
B) L
C) 2L
D) L/√2
Ans: A -
Column with one end fixed and other free has effective length
A) 2L ✔️
B) L
C) L/2
D) √2L
Ans: A