1) The shear stress distribution over a rectangular cross section of a beam follows
a) a straight line path
b) a circular path
c) a parabolic path
d) an elliptical path
a) a straight line path
b) a circular path
c) a parabolic path
d) an elliptical path
a) Mohr's theory
b) Rankine's theory
c) Maximum strain theory
d) Maximum shear energy theory
a) proportional limit
b) elastic limit
c) tolerance limit
d) endurance limit
a) creep
b) toughness
c) strength
d) hardness
a) fatigue
b) creep
c) resilience
d) plasticity
a) plasticity
b) fatigue
c) resilience
d) creep
a) limit of proportionality
b) elastic limit
c) plastic limit
d) none of above
a) rectangle
b) triangle
c) hexagon
d) square
a) lies between 0 and 140
b) lies between 0 and 100
c) is less than 80
d) has any value
a) both ends are hinged
b) both ends are fixed
c) one is fixed and other end is hinged
d) one end is fixed and other end is free
a) length of column only
b) least lateral dimension only
c) both length and least lateral dimension
d) none of the above
a) bending stress
b) deflection
c) stiffness
d) bending moment
a) shear stress to shear strain
b) stress to strain
c) longitudinal stress to longitudinal strain
d) stress to volumetric strain
a) decrease
b) remain unchanged
c) increase to two times
d) increase to four times
a) homogeneous
b) isotropic
c) orthotropic
d) elastic
a) that of a prismatic bar of same length
b) one half that of a prismatic bar of same length
c) one third that of a prismatic bar of same length
d) one fourth that of a prismatic bar of same length
a) shear
b) tension
c) compression
d) torsion
a) quadratic parabola
b) cubic parabola
c) catenary
d) arc of a circle
a) at the neutral axis
b) at the base
c) above the neutral axis
d) below the neutral axis
a) two times
b) four times
c) eight times
d) sixteen times
a) greater than 80
b) less than 80
c) greater than 180
d) greater than 129
a) 0.5 x stress x strain x volume
b) 0.5 x stress x volume
c) 0.5 x stress x strain
d) 0.5 x strain x volume
a) 1/4 times
b) 1/8 times
c) 4 times
d) 8 times
a) maximum shear stress theory
b) maximum primcipal strain theory
c) shear strain energy theory
d) maximum principal stress theory
a) pure shear
b) uniaxial stress only
c) equal and opposite axial stresses on two mutually perpendicular planes, the planes being free of shear
d) equal axial stresses on two mutually perpendicular planes, the planes being free of shear
a) for a given level of stress, the rate of creep is independent of time
b) creep is time dependent deformation under stress
c) creep is deformation due to high temperature under no stress condition
d) creep is independent of temperature
a) ellipse
b) rectangle
c) hexagon
d) circle
a) simply supported beam
b) fixed beam
c) continuous beam
d) cantilever beam
a) normal thrust and shear force
b) shear force and bending moment
c) normal thrust and bending moment
d) normal thrust, shear force and bending mement
a) to reduce bending moment throughout
b) to increase bending moment throughout
c) to increase shear force
d) to decrease shear force
a) circular sect. is more economical
b) square sect. is more economical
c) both sections are equally strong
d) both sections are equally stiff
a) 9
b) 2
c) 1
d) 3
a) last 25% of deformation
b) elastic deformation
c) non- elastic deformation
d) 50% of total deformation
a) reciprocal of normal strain within elastic limit
b) normal strain within proportional limit
c) normal strain withim elastic limit
d) normal strain at yield point
a) ductility
b) yield stress
c) ultimate strength
d) strength
a) one end hinge and other on rollers
b) one end fixed and the other on rollers
c) both ends on rollers
d) one end fixed and the other free
a) the S.F. is uniform
b) the S.F. is maximum
c) the S.F. is zero
d) none of these
a) flexural rigidity
b) torsional rigidity
c) second moment of area
d) none of these
a) the property by which a body returns to its original shape after removal of load
b) the ratio of stress to strain
c) large deformability as in case of rubber
d) the resistance of the force acting
a) a body of such a material with a lot of extensibility
b) a body made of rubber only
c) that body which recovers its original shape completely after removal of force
d) a body whose cross-sectional dimensions are very small
a) irrecoverable deformation in the body
b) the force which acts permanently on the body
c) the shape of the member just after completion of construction
d) ratio of Poisson's Ratio to Young's Modulus
a) 1.0
b) 1.25
c) 0.50
d) 1.5
a) N/m2
b) N/cm2
c) Pascal
d) both (a) and (c)
a) N/cm2
b) kg/cm2
c) dyne/cm2
d) erg
a) minimum
b) maximum
c) same as at the center
d) zero
a) resilience
b) work modulus
c) resistance
d) virtual work
a) N/cm2
b) N/m2
c) dyne/cm2
d) no units
a) <100
b) 0
c) >120
d) >120 but less than 180
a) ultimate impact strength
b) ultimate shear strength
c) ultimate strength in compression
d) ultimate strength in tension
a) bending stresses
b) axial tension
c) axial compressive stress
d) shear stresses
a) the resistance offered by the material per unit area to a force
b) load per unit area
c) continued deformation under sustained loading
d) the strain per unit length
a) Poisson
b) Robert Hook
c) Thomas Young
d) Mohr
a) lateral strain to longitudinal strain
b) laterial elongation to linear elongation
c) lateral stress to linear stress
d) Young's Modulus of elasticity to Modulus of Rigidity
a) ultimate strength
b) stress corresponding to 0.2% strain from the stress strain curve
c) average of ultimate strength and actual breaking stress
d) the stress at which the permanent set reaches the value 0.2%
a) they can be made of good material
b) they can be easily analysed
c) higher loads can be supported with less consumption of material
d) they can be designed to have larger dimensions
a) fail after giving ample warning
b) fail suddenly
c) never fail
d) never be used for structural purposes
a) to become brittle
b) disappearance of deformation on removal of load
c) continued deformation with time under sustained loading
d) not being ductile
a) the failure occurs by crushing of the material
b) the column is having initial curvature and the load is eccentrically applied
c) the column shortens so much that it will become a short column
d) the failure occurs by buckling omly
a) effective length only
b) the ultimate crushing strength of the material
c) radius of gyration only
d) the maximum slenderness ratio
a) 4
b) 2
c) 6
d) 8
a) factor of safety crippling load x safe load
b) factor of safety crippling load / safe load
c) factor of safety crippling load - safe load
d) factor of safety z: safe load/ crippling load
a) length of the column
b) diameter of the column
c) moment of inertia of the column
d) none of these
a) one and a half
b) three
c) two
d) four
a) ratio of linear stress to linear strain
b) ratio of shear stress to shear strain
c) ratio of lateral strain to longitudinal strain
d) ratio of the normal stress ( of equal magnitude on all six faces ) on a solid cube to the volumetric strain
a) ratio of linear stress to linear strain
b) ratio of shear stress to shear strain
c) ratio of lateral strain to longitudinal strain
d) ratio of the normal stress ( of equal magnitude on all six faces ) on a solid cube to the volumetric strain
a) ratio of linear stress to linear strain
b) ratio of shear stress to shear strain
c) ratio of lateral strain to longitudinal strain
d) ratio of the normal stress ( of equal magnitude on all six faces ) on a solid cube to the volumetric strain
a) elasticity
b) plasticity
c) ductility
d) resilience
a) ratio of linear stress to linear strain
b) ratio of shear stress to shear strain
c) ratio of lateral strain to longitudinal strain
d) ratio of the normal stress ( of equal magnitude on all six faces ) on a solid cube to the volumetric strain
a) ultimate load to load at yield
b) yield stress to working stress
c) ultimate strength to yield stress
d) working stress to yield stress
a) malleability
b) elasticity
c) ductility
d) brittleness
a) length of the member
b) area of cross-section
c) supporting conditions at the two ends
d) none of above
a) same strain
b) same stress
c) equal areas
d) same Young's Modulus
a) 5.65
b) 6.56
c) 7.75
d) 6.65
a) circular
b) square
c) rectangle
d) none of the above
a) M
b) 2M
c) 3M
d) 4M
a) crest point
b) point of inflation
c) neutral point
d) point of contraflexure
a) strain in all the material is same
b) the sum of the individual loads carried by different materials is equal to the external load
c) both (a) and (b)
d) none of the above
a) high carbon steel
b) bronze
c) cast iron
d) mild steel
a) increase
b) decrease
c) not be affected
d) difficult to tell
a) decrease
b) not be affected
c) increase
d) become zero
a) copper
b) timber
c) brass
d) mild steel
a) inclined loads with moments
b) purely vertical loading
c) purely inclined loads
d) any general loading
a) inclined at 45o to the direction of tensile stress applied
b) perpendicular to the direction of tensile stress applied
c) along the direction of tensile stress
d) none of the above
a) 2
b) 3
c) 8
d) 4
a) when it carries a concentrated load at mid span
b) when it carries a concentrated load at the end
c) when it carries a u.d.l. , over the entire span
d) none of the above
a) 45o
b) 30o
c) 90o
d) 0o
a) 0o
b) 45o
c) 90o
d) 30o
a) 60o
b) 30o
c) 45o
d) 90o
a) maximum normal stress
b) minimum shear stress
c) maximum shear stress
d) minimum normal stress
a) maximum shear stress
b) maximum normal stress
c) minimum normal stress
d) none of the above
a) 0.5
b) 4
c) 2.5
d) 0.4
a) 0.5
b) 1.0
c) 0
d) 1.5
a) pure shear stress
b) normal tensile stress
c) bending stress
d) normal compressive stress
a) 0
b) 1
c) 2
d) 3
a) the bending moment at that section
b) the ordinate of loading diagram at that section
c) the area of loading diagram from end to that section
d) the slope of loading at that section
a) twice the moment of inertia about the centroidal axis
b) three times the moment of inertia about the centroidal axis
c) four times the moment of inertia about the centroidal axis
d) none of the above
a) additional rivets are provided
b) welding is done
c) the thickness of each plate will be changing
d) the width of the plate will be gradually decreased
a) slope at the section
b) S.F. at the section
c) load intensity at the section
d) B.M. at the section
a) greater than 3
b) 0
c) less than 3
d) 3
a) parabola with wl/4 max. ordinate
b) triangle with wl2/8 max. ordinate
c) rectangle with uniform ordinate wl2/8
d) parabola with wl2/8 max. ordinate
a) any general loading
b) loading with no component perpendicular to the direction of beam
c) only when no load except self weight acts
d) loading with no component in the direction of the beam