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A. Cantilever beam
B. Simply supported beam
C. Fixed beam
D. Continuous beam
A. Free from corrosion
B. Free from stresses
C. Stronger in tension
D. Leak-proof
A. False
B. True
A. Single riveted
B. Double riveted
A. Short column
B. Medium column
C. Weak column
D. Long column
A. Maximum
B. Infinity
C. Minimum
D. Zero
A. Isotropic material
B. Homogeneous material
C. Hetrogeneous material
D. Composite material
A. The axis of load
B. Would not occur
C. At right angles to the axis of specimen
D. An oblique plane
A. Shear stress
B. Strain
C. Tensile stress
D. Compressive stress
A. Measure linear strain
B. Relieve strain
C. Measure volumetric strain
D. Measure shear strain
A. Depends
B. Does not depend
A. 2
B. 1/8
C. 1/4
D. 4
A. Equal to
B. Twice
C. Four times
D. One-half
A. Proof resilience
B. Resilience
C. Impact energy
D. Strain energy
A. Direct and bending stress both
B. Direct stress only
C. Shear stress only
D. Bending stress only
A. Same
B. Double
C. Six times
D. Four times
A. Anywhere
B. Middle
C. Larger end
D. Smaller end
A. Bending moment changes sign
B. Bending moment is maximum
C. Shear force is maximum
D. Shear force changes sign
A. Top layer
B. Every cross-section
C. Bottom layer
D. Neutral axis
A. True
B. False
A. Small castings
B. Large scale production of castings
C. Large castings
D. Complicated castings
A. Voltage limiter
B. Current limiter
C. Short circuit
D. Voltage regulator
A. Metallurgy
B. Mechanics of materials
C. Engineering materials
D. Properties of materials
E. Strength of materials
A. Thermodynamics
B. Mechanics
C. Physics
D. Strength of materials
A. Height of a material's Young's modulus
B. Volume of a material
C. Amount of stress within a material
D. Size of the material
E. Ability to withstand an applied load without failure
A. Elasticity
B. Density
C. Strength
D. Toughness
A. Kilopols
B. Joules
C. Pounds per square inch
D. Millimeters of mercury
E. Hertz
A. Tension
B. Pressure
C. Elongation
D. Stress
E. Area
A. Elasticity
B. Inch
C. Young's modulus
D. Dimensionless
E. Pound
A. Critical stress
B. Maximum stress
C. Hysteresis
D. Proportional limit
E. Linearity
A. Shear stress
B. Damage limit
C. Fracture
D. Elastic limit
E. Tensile stress
A. When the strain energy is greater than the elastic limit
B. When the working stress exceeds the elastic limit
C. When a permanent deformation occurs
D. When the working stress does not exceed the elastic limit
E. When the stress decreases with increasing strain
A. Elongation point
B. Yield point
C. Elastic limit
D. Hardening point
E. Fracture
A. A point on the yield-fracture line
B. A physical characteristic of a material
C. The intersection of the yield and fracture curves
D. A location on a graph
E. A point on the stress-strain curve
A. Yield strength
B. Ultimate tensile strength
C. Shear strength
D. Tensile strength
A. Newton's Third Law of Motion
B. The First Law of Thermodynamics
C. Hooke's Law
D. The Law of Vibrations
E. Laplace's Law
A. Proportional limit
B. Ultimate limit
C. Ultimate strength
D. Shear stress
E. Strength limit
A. The probability of failure
B. The likelihood of failure
C. The number of failure points
D. The number of failures
E. The value
A. Maximum Calories
B. Ultimate strength
C. Maximum effort
D. The height of Mount Everest
A. Elastic limit
B. Shear modulus
C. Ultimate tensile strength
D. Failure point
A. Chemical
B. Nuclear
C. Inertial
D. Pushing
E. Elastic
A. Its porosity
B. Its width
C. Its thickness
D. Its origin shape or length
E. Its grain size
A. Alliance
B. Bending
C. Shear
D. Tensile
A. Point of failure
B. Maximum stress point
C. Point at which material exceeds the elastic limit
D. Maximum stress that a material can withstand
A. Frequency of earthquakes
B. Amount of bacteria in a sample
C. Lateral to longitudinal strain
D. Amount of blood in an artery
E. Amount of noise in an image
A. Metal
B. Surface
C. Sheath
D. Metal Core
A. Neutral axis
B. Interface
C. Interface line
D. Perpendicular
E. Parallel
A. Equal stress for all runs
B. Equal stress on all axes
C. Zero stress
A. Crushing
B. Rupture
C. Shearing
D. Yielding
E. Fracture
A. Design stress
B. Shear stress
C. Ultimate stress
A. Change in volume to original volume
B. Change in length to original length
C. Change in cross-sectional area to original cross-sectional area
D. Any one of the above
E. None of the above.
A. Yield point
B. Limit of proportionality
C. Breaking point
D. Elastic limit
E. Plastic limit.
A. Volumetric stress and volumetric strain
B. Lateral stress and lateral strain
C. Longitudinal stress and longitudinal strain
D. Shear stress to shear strain
E. Longitudinal stress and lateral strain.
A. Mm/mm
B. Kg/cm
C. Kg
D. Kg/cm2
E. Kg cm2.
A. Strain
B. Lateral strain
C. Linear strain
D. Linear stress
E. Unit strain.
A. Internal resistanpe
B. Tensile stress
C. Transverse stress
D. Compressive stress
E. Working stress.
A. Ideal materials
B. Uniform materials
C. Isotropic materials
D. Paractical materials
E. Elastic materials.
A. Uniform throughout
B. Increase uniformly
C. First increase and then decrease
D. Increase uniformly first and then increase rapidly
E. Increase rapidly first and then uniformly.
A. Longitudinal stress and longitudinal strain
B. Volumetric stress and volumetric strain
C. Lateral stress and lateral strain
D. Shear stress and shear strain
E. Linear stress and lateral strain.
A. Doubled
B. Halved
C. Become four times
D. Become one-fourth
E. Remain unaffecte
A. Same
B. More
C. Less
D. More or less depending on other factors
E. Unpredictable.
A. Area at the time of fracture
B. Original cross-sectional area
C. Average of and
D. Minimum area after fracture
E. None of the above.
A. Toughness
B. Tensile strength
C. Capability of being cold worked
D. Hardness
E. Fatigue strength.
A. Half
B. Same amount
C. Double
D. One-fourth
E. Four times.
A. 50%
B. 25%
C. 0%
D. 15%
E. 60%.
A. Unit stress
B. Bulk modulus
C. Modulus of rigidity
D. Modulus of elasticity
E. Principal stress.
A. Load/original cross-sectional area and change in length/original length
B. Load/instantaneous cross-sectional area original area and log.
C. Load/instantaneous cross-sectional area and change in length/original length
D. Load/instantaneous area and instantaneous area/original area
E. None of the above.
A. 4 tonnes/cm2
B. 8 tonnes/cm2
C. 16 tonnes/cm2
D. 22 tonnes/cm2
E. None of the above.
A. Same
B. Half
C. One-third
D. Two-third
E. One-fourth.
A. Kinematic viscosity
B. Surface tension
C. Bulk modulus
D. Strain
E. Elasticity.
A. It does not exist
B. It is more sensitive to changes in both metallurgical and mechanical conditions
C. It gives, a more accurate picture of the ductility
D. It can be correlated with stress-strain values in other tests like torsion, impact, combined stress tests et
E. It can be used for compression tests as well.
A. More
B. Less
C. Same
D. More/less depending on composition
E. May have any value.
A. Principal stress
B. Tensile stress
C. Compressive stress
D. Shear stress
E. No stress.
A. Rubber
B. Plastic
C. Brass
D. Steel
E. Glass.
A. 2.1xl05 kg/cm2
B. 2.1 X 106 kg/cm2
C. 2.1 x 107 kg/cm2
D. 0.1 xlO6 kg/cm2 () 3.8 x 106 kg/cm2.
A. 0.01 to 0.1
B. 0.23 to 0.27
C. 0.25 to 0.33
D. 0.4 to 0.6
E. 3 to 4.
A. Slenderness ratio and area of cross-section
B. Poisson’s ratio and modulus of elasticity
C. Slenderness ratio and modulus of elasticity
D. Slenderness ratio, area of cross-section and modulus of elasticity
E. Poisson’s ratio and slenderness ratio.
A. Of same magnitude as that of bar and applied at the lower end
B. Half the weight of bar applied at lower end
C. Half of the square of weight of bar applied at lower end
D. One-fourth of weight of bar applied at lower end
E. None of the above.
A. Plasticity
B. Elasticity
C. Ductility
D. Malleability
E. Resilience.
A. Homogeneous
B. Inelastic
C. Isotropic
D. Isentropic
E. Visco-elasti
A. 0.1 to 0.2
B. 0.23 to 0.27
C. 0.25 to 0.33
D. 0.4 to 0.6
E. 3 to 4.
A. Plasticity
B. Ductility
C. Elasticity
D. Malleability
E. Drawabihty.
A. Longitudinal stress and longitudinal strain
B. Longitudinal stress and lateral stress
C. Lateral stress and longitudinal stress
D. Lateral stress and lateral strain
E. None of the above.
A. Steel
B. Copper
C. Aluminium
D. Cast iron
E. None of the above.
A. Malleability
B. Ductility
C. Plasticity
D. Elasticity
E. Reliability.
A. Increase
B. Decrease
C. Remain same
D. Increase initially and then decrease
E. Unpredictable.
A. More than 50%
B. 25—50%
C. 10—25%
D. 5—10%
E. Negligible.
A. Thermal stresses
B. Tensile stress
C. Bending
D. Compressive stress
E. No stress.
A. Tensile strain increases more quickly
B. Tensile strain decreases more quickly
C. Tensile strain increases in proportion to the stress
D. Tensile strain decreases in proportion to the stress
E. Tensile strain remains constant.
A. Considerably greater than that necessary to continue it
B. Considerably lesser than that necessary to continue it
C. Greater than that necessary to stop it
D. Lesser than that necessary to stop it
E. Equal to that necessary to stop it.
A. Creeping
B. Yielding
C. Breaking
D. Plasticity
E. None of the above.
A. Breaking stress
B. Fracture stress
C. Yield point stress
D. Ultimate tensile stress
E. Proof stress.
A. Breaking stress
B. Maximum load/original cross-sectional area
C. Load at breaking point/A
D. Load at breaking point/neck area
E. Maximum stress.
A. Ultimate tensile stress
B. Proof stress
C. Stress at yield point
D. Stress at elastic limit
E. Tensile stress.
A. Young’s modulus
B. Bulk modulus
C. Modulus of rigidity
D. Modulus of elasticity
E. Poisson’s ratio.
A. Young’s modulus
B. Bulk modulus
C. Modulus of rigidity
D. Modulus of elasticity
E. Poisson’s ratio.
A. Same in both cases
B. Zero in first case
C. Different in both cases
D. Data are not sufficient to determine same
E. None of the above.
A. Fluids in motion
B. Breaking point
C. Plastic deformation of solids
D. Rupture stress
E. None of the above.
A. Not deform
B. Be safest
C. Stretch
D. Not stretch
E. None of the above.
A. Strain energy
B. Resilience
C. Proof resilience
D. Modulus of resilience
E. Toughness.