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4

If fbt and fc are the co-existent bending tensile stress and shear stress in a member, the equivalent stress fc is

A. √(fbt² + fc²)

B. √(fbt² + ½fc²)

C. √(fbt² + 3fc²)

D. √(fbt² - 3fc²)

Correct Answer :

C. √(fbt² + 3fc²)


Related Questions

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4

For the buildings having a low permeability, the internal wind pressure acting normal to the wall and roof surfaces is taken as

A. Zero

B. ±0.2 p

C. ± 0.5 p

D. ±0.7 p Where p is basic wind pressure

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4

The internal pressure coefficient on walls for buildings with large permeability is taken as

A. ± 0.2

B. ±0.5

C. ± 0.7

D. 0

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4

If d is the distance between the flange angles,

A. Vertical stiffeners are provided in steel plate girders if the web is less than d/85

B. Vertical stiffeners are provided in high tensile steel plate girders if the web is less than d/175

C. Horizontal stiffeners are provided in steel plate girders if the web is less than d/200

D. All the above

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4

Gantry girders are designed to resist

A. Lateral loads

B. Longitudinal loads and vertical loads

C. Lateral, longitudinal and vertical loads

D. Lateral and longitudinal loads

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4

A butt weld is specified by

A. Effective throat thickness

B. Plate thickness

C. Size of weld

D. Penetration thickness

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4

Spans of continuous fillers are considered approximately equal if the longest span does not exceed the shortest span by more than

A. 5 %

B. 10 %

C. 15 %

D. 20 %

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4

In a built up beam actual bending compressive stress fbc is given by (when y1 is the distance of the edge of the beam from the neutral axis).

A. fbc = (M/Ixx) × y₁

B. fbc = (Ixx/M) × y₁

C. fbc = (Ixx/M) + y₁

D. fbc = (M/Ixx) + y₁

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4

The bracing provided in the plane of end posts is called

A. Sway bracing

B. Portal bracing

C. Top lateral bracing

D. Bottom lateral bracing

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4

The difference between gross diameter and nominal diameter for the rivets up to 25 mm diameter is

A. 1.0 mm

B. 1.5 mm

C. 2.0 mm

D. 2.5 mm

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4

A beam is defined as a structural member subjected to

A. Axial loading

B. Transverse loading

C. Axial and transverse loading

D. None of these

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4

When the upper column does not provide full bearing area over lower column, the column splice is provided with the following assumption

A. Bearing plate is assumed as a short beam to transmit the axial load to the lower column section

B. Axial load is assumed to be taken by flanges

C. Load transmitted from the flanges of upper column and reactions from the flanges of lower columns are equal and form a couple

D. All the above

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4

For a standard 45° fillet, the ratio of size of fillet to throat thickness is

A. 1 : 1

B. 1 : √2

C. √2 : 1

D. 2 : 1

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4

The statical method of plastic analysis satisfies

A. Equilibrium and mechanism conditions

B. Equilibrium and plastic moment conditions

C. Mechanism and plastic moment conditions

D. Equilibrium condition only

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4

The maximum axial load which is just sufficient to keep a column in a small deflected shape, is called

A. Crippling load

B. Buckling load

C. Critical load

D. All the above

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4

The maximum tensile and compressive bending stress in extreme fibres of rolled I-sections and channels on the effective section, is

A. 1500 kg/cm2

B. 1420 kg/cm2

C. 1650 kg/cm2

D. 2285 kg/cm2

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4

In case of timber structures, the simple bending formula M = fz may be applied for

A. Rectangular beams up to 300 mm depth

B. All rectangular beams

C. Solid circular beams only

D. All square cross-section beams

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4

With usual notations of the letters, the shear stress fs at any point of the cross-section is given by

A. fs =FQ/It

B. fs =Ft/IQ

C. fs =It/FQ

D. fs =IF/Qt

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4

The thickness of the web of a mild steel plate girder is less than d/200. If only one horizontal stiffener is used, it is placed at

A. The neutral axis of the section

B. 2/3rd of the depth of the neutral axis from the compression flange

C. 2/5th of the depth of the neutral axis from the compression flange

D. 2/5th of the height of the neutral axis from tension flange

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4

For a cantilever beam of length L built-in at the support and restrained against torsion at the free end, the effective projecting length l is

A. l = 0.7 L

B. l = 0.75 L

C. l = 0.85 L

D. l = 0.5 L

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4

Rolled steel beams are:

A. Mainly used to resist bending stress

B. Used as independent sections to resist compressive stress

C. Used as independent sections to resist tensile stress

D. All the above

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4

If L is the overall length of a combined footing having A as its area, d being the distance between the centre of gravity of the base and centre of the base, the larger width b is

A. (A/L) + (3Ad/L²)

B. (A/L) + (6Ad/L²)

C. (A/L) - (6Ad/L²)

D. (A/L) - (3Ad/L²)

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4

Secant formula for direct stress in compression, is applicable only for slenderness ratio upto

A. 120

B. 130

C. 140

D. 150

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4

The gross section of the web of a beam is defined as

A. Depth of the beam multiplied by its web thickness

B. Width of the flange multiplied by its web thickness

C. Sum of the flange width and depth of the beam multiplied by the web thickness

D. None of these

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4

The minimum width B of a solid casing for a cased beam, is equal to

A. B = b + 25 mm

B. B = b + 50 mm

C. B = b + 75 mm

D. B = b + 100 mm

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4

Select the correct statement

A. Material cost of a rivet is higher than that of a bolt

B. Tensile strength of a bolt is lesser than that of a rivet

C. Bolts are used as a temporary fastening whereas rivets are used as permanent fastenings

D. Riveting is less noisy than bolting

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4

Bearing stiffener in a plate girder is used to

A. Transfer the load from the top flange to the bottom one

B. Prevent buckling of web

C. Decrease the effective depth of web

D. Prevent excessive deflection

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4

As compared to field rivets, the shop rivets are

A. Stronger

B. Weaker

C. Equally strong

D. Any of the above

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4

The range of economical spacing of trusses varies from

A. L/3 to L/5

B. L/4 to 2L/5

C. L/3 to L/2

D. 2L/5 to 3L/5, where L is span

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4

The effective length of a compression member of length L held in position and restrained in direction at one end and effectively restrained in direction but not held in position at the other end, is

A. L

B. 0.67 L

C. 0.85 L

D. 1.5 L

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4

Slenderness ratio of a compression member is

A. Moment of inertia/Radius of gyration

B. Effective length/Area of cross-section

C. Radius of gyration/Effective length

D. Radius of gyration/ Area of cross-section