Question #64290

A beam, 3 m long is freely supported at it's ends and carries a uniformly distributed load of 2,4 kN/m run from B to it's centre. Draw the shearing force and bending moment diagram and give the magnitude and position of the maximum bending moment

Expert's answer

Answer on Question #64290-Engineering-Civil and Environmental Engineering

A beam, 3m3\mathrm{m} long is freely supported at its ends and carries a uniformly distributed load of 2.4kN/m2.4\mathrm{kN / m} run from B to its center. Draw the shearing force and bending moment diagram and give the magnitude and position of the maximum bending moment

Solution

Free-Body-Diagram

The shearing force and bending moment diagram


The magnitude and position of the maximum bending moment: 1.52 kNm at 1.88 m.

1. A beam is in equilibrium when it is stationary relative to an inertial reference frame. The following conditions are satisfied when a beam, acted upon by a system of forces and moments, is in equilibrium:


ΣFx=0:HB=0\Sigma F _ {x} = 0: H _ {B} = 0

ΣMA=0\Sigma M_A = 0 : The sum of the moments about a point AA is zero:


q11.5(1.5+1.52)+RB3=0- q _ {1} 1. 5 \left(1. 5 + \frac {1 . 5}{2}\right) + R _ {B} 3 = 0

ΣMB=0\Sigma M_{B}=0: The sum of the moments about a point B is zero:

RA3+q11.5(1.51.52)=0-R_{A}3+q_{1}1.5\left(1.5-\frac{1.5}{2}\right)=0

2. Solve this system of equations:

HB=0  (kN)H_{B}=0\;(kN)

Calculate reaction of pin support about point B:

RB=q11.5(1.5+1.52)3=2.41.5(1.5+1.52)3=2.70  (kN)RB=\frac{q_{1}1.5\left(1.5+\frac{1.5}{2}\right)}{3}=\frac{2.4\cdot 1.5\left(1.5+\frac{1.5}{2}\right)}{3}=2.70\;(kN)

Calculate reaction of roller support about point A:

RA=q11.5(1.51.52)3=2.41.5(1.51.52)3=0.90  (kN)RA=\frac{q_{1}1.5\left(1.5-\frac{1.5}{2}\right)}{3}=\frac{2.4\cdot 1.5\left(1.5-\frac{1.5}{2}\right)}{3}=0.90\;(kN)

3. The sum of the forces is zero:

ΣFy=0\Sigma F_{y}=0: RAq11.5+RB=0.902.41.5+2.70=0R_{A}-q_{1}1.5+R_{B}=0.90-2.4\cdot 1.5+2.70=0

Draw diagrams for the beam

First span of the beam: 0x1<1.50\leq x_{1}<1.5

Determine the equations for the shear force (Q):

Q(x1)=RAQ(x_{1})=R_{A}

Q1(0)=0.90=0.90  (kN)Q1(0)=0.90=0.90\;(kN)

Q1(1.50)=0.90=0.90  (kN)Q1(1.50)=0.90=0.90\;(kN)

Determine the equations for the bending moment (M):

M(x1)=RA(x1)M(x_{1})=R_{A}(x_{1})

M1(0)=0.90(0)=0  (kNm)M_{1}(0)=0.90(0)=0\;(kNm)

M1(1.50)=0.90(1.50)=1.35  (kNm)M_{1}(1.50)=0.90(1.50)=1.35\;(kNm)

Second span of the beam: 1.5x2<31.5\leq x_{2}<3

Determine the equations for the shear force (Q):

Q(x2)=RAq1(x21.5)Q(x_{2})=RA-q_{1}(x_{2}-1.5)

Q2(1.50)=0.902.40(1.51.5)=0.90  (kN)Q_{2}(1.50)=0.90-2.40(1.5-1.5)=0.90\;(kN)

Q2(3)=0.902.40(31.5)=2.70  (kN)Q_{2}(3)=0.90-2.40(3-1.5)=-2.70\;(kN)

The value of Q on this span that crosses the horizontal axis. Intersection point:

x=0.38x=0.38

Determine the equations for the bending moment (M):


M(x2)=RA(x2)q1(x21.5)22M(x_2) = R_A(x_2) - \frac{q_1 (x_2 - 1.5)^2}{2}M2(1.50)=0.90(1.50)2.40(1.501.5)22=1.35(kNm)M_2(1.50) = 0.90(1.50) - \frac{2.40(1.50 - 1.5)^2}{2} = 1.35\,(\text{kNm})M2(3)=0.90(3)2.40(31.5)22=0(kNm)M_2(3) = 0.90(3) - \frac{2.40(3 - 1.5)^2}{2} = 0\,(\text{kNm})


Local extremum at the point x=0.38x = 0.38:


M2(1.88)=0.90(1.88)2.40(1.881.5)22=1.52(kNm)M_2(1.88) = 0.90(1.88) - \frac{2.40(1.88 - 1.5)^2}{2} = 1.52\,(\text{kNm})


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