Strength of Materials (GATE Aerospace and GATE ......o Cantilever beam Cantilever with an end point...

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Contact- 9740501604 Strength of Materials (GATE Aerospace and GATE Mechanical) By Mr Dinesh Kumar

Transcript of Strength of Materials (GATE Aerospace and GATE ......o Cantilever beam Cantilever with an end point...

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Strength of Materials

(GATE Aerospace and GATE Mechanical) By

Mr Dinesh Kumar

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Shear Forces and Bending Moments

A slender structural member is usually classified according to the types of loads, they support. For example, a beam is a type of structural member subjected to transverse loads, that is, forces or moments having their vectors perpendicular to the axis of the bar.

Type of supports :-

o Fixed support

o Hinge support or pinned support

→ u=v = 0

→ 휃 = 0

→ Force ≠0

→ Moment ≠0

→ Shear stress ≠0

→ Bending stress ≠0

→ u=v = 0

→ 휃 ≠ 0

→ Force ≠0

→ Moment =0

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o Roller support

Types of Beams:-

o Simply supported Beam

→ v = 0

→ u ≠ 0

→ 휃 ≠ 0

→ Force ≠0

→ Moment =0

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o Cantilever beam

o Beam with overhang

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o Propped Cantilever beam

o o Fixed beam

o Continuous beam

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Type of load o Concentrated load

o Uniformly distributed load (UDL)

o Uniformly varying load (VDL)

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o Concentrated moment

]

Sign convention of shear force and bending moment

Consider the sign conventions for shear forces and bending moments.

According to above figure, a positive shear force acts clockwise against the material and a negative shear force acts counterclockwise against the material. Also, a positive bending (sagging) moment compresses the upper part of the beam and a negative bending (hogging) moment compresses the lower part.

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Relationship between loads, shear force and bending moments Consider a small section of beam of length dx as shown in the figure, it is subjected to a udl of intensity of q(x) as shown. Free body dia for shear forces and bending moment as shown.

o Force equilibrium In Vertical direction ∑F = 0 q(x)dx – V + (V+dV) = 0 q(x)dx + dV = 0 q(x) = - 풅푽

풅풙

o Moment equilibrium

Taking Moment equilibrium about z axis passing through CG of the section

∑M = 0

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Vdx + M + (V+ dV) dx – M – dM = 0 V푑푥+ Vdx + dV dx – dM = 0 (here 푑푣푑푥 is very small) Vdx – dM = 0 V = 풅푴

풅풙

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Shear- force and bending moment diagrams o Cantilever beam

Cantilever with an end point lod

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Cantilever with UDL

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Cantilever with point load at mid-span and UDL

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Cantilever with moment at mid-span and UDL

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Simply supported beam o Simply supported beam with point load

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o Simply supported beam with UDL

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Problems

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3.

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5.

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