B. 7.5 mm
C. 5 mm
D. 15 mm
A. Two times
B. Three times
D. Five times
A. R + T
C. T R
D. R T
A. WL/P
B. WL/2P
C. WL/4P
A. (1 C)mf + eE
B. (1 C) mf eE
C. (C 1)mf eE
A. To provide high bond stresses
C. To overcome high bearing stresses developed at the ends
D. To overcome bursting stresses at the ends
A. 0.1 L from the outer edge of column
B. One -fourth the distance of projection
D. Half the distance of projection
A. Its own weight
B. Load of the surcharge, if any
C. Weight of the soil above it
A. Drop panel
B. Supporting end of the column
D. Top of the column
B. Resist the temperature stresses
C. Distribute the load
D. Resist the shrinkage stress
B. h W/Aw) [(1 )/(1 + sin )]
C. h = (W/Aw) [(1 + )/(1 + sin )]
D. h = (W/Aw) [(1
B. Is increased by Pe/Z
C. Is increased by PZ/e
D. Remains unchanged
B. D = 0.775 a
C. D = 0.0775 a
D. D = 0.775 a2
B. Also considered for calculating the upward pressure on footing
C. Not considered for calculating the area of the footing
D. Both B. and C
A. Below the slab
B. At the bottom edge of the slab
D. Within the flange
A. Square
C. Octagonal
D. Circular
B. 3 diameters
C. 2.5 diameters
D. 3.5 diameters
A. 10 mm
B. 15 mm
C. 20 mm
A. 18 mm diameter
B. 24 mm diameter
D. 30 mm diameter
A. 2
C. [(p p p p cos 2
D. [(p p p p /2] sin 2
E. [(p p p p to the principal plane carrying the principal stress p1, is:
A. Rankine formula
C. Marcus formula
D. Grashoff formula
A. One and half lever arm of the section
B. One -half lever arm of the section
D. One-third lever arm of the section
A. Half of the width of the slab
C. Two -third of the width of the slab
D. Four-fifth of the width of the slab
A. Hooked splice
B. Straight bar splice
D. Dowel splice
B. Smaller of 25 mm or diameter
C. Smaller of 40 mm or diameter
D. Greater of 40 mm or diameter
A. 20
C. 25
D. 35
A. None of these
B. Simply supported beam
D. Continuous beam
A. Increasing the total perimeter of bars
C. Decreasing the lever arm
D. Replacing smaller bars by greater number of greater bars
A. B.M = pb (b + a)/8
B. B.M = pb (b a)/4
D. B.M = pb (c a)/4
B. Kept uniform throughout
C. Kept zero at the edge
D. Increased gradually towards the edge
A. Decreased towards the centre of the beam
B. Increased at the ends
D. Kept constant throughout the length
B. Five times
C. Four times
D. Three times
A. L/36 for end panels without drops
C. L/32 for end panels without drops
D. L/36 for interior panels without drop
A. 2WR/16
B. 3WR/16
D. None of these
A. Is safe in shear
B. Is safe with stirrups and inclined bars
C. Is safe with stirrups
B. A key
C. A rib
D. A cut-off wall
A. Elastic shortening of concrete
B. Shrinkage of concrete
D. Creep of concrete
A. 0.6
C. 0.8
D. 0.7
A. ( h
C. [( + )/4] h
D. [( )/2] h
B. Trapezoidal
C. Square
D. Triangular
B. m = 3500/3C
C. m = 700/3C
D. m = 1400/3C
A. t; NON OF THESE
B. 5WR/16
D. 2WR/16
B. None of these
C. Stress in steel area of steel
D. Stress in concrete area of concrete
A. Sixteen times the diameter of the smallest longitudinal reinforcing rods in the column
B. Forty-eight times the diameter of transverse reinforcement
D. The least lateral dimension of the column
A. A/P
B. P/2A
C. 2A/P
A. One- sixth of the effective span
C. Breadth of the rib + four times thickness of the slab
D. Breadth of the rib + half clear distance between ribs
A. h/2
B. h /4
D. 2h/3
A. Is safe with stirrups
B. Is safe with stirrups and inclined members
C. Needs revision of the section
A. Removal of cracks in the members due to shrinkage
B. Its dimensions are not decided from the diagonal tensile stress
D. Large size of long beams carrying large shear force need not be adopted
A. 0.5% and not more than 5% of cross-sectional area
C. 0.6% and not more than 6% of cross-sectional area
D. 0.7% and not more than 7% of cross-sectional area
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