Mechanical Engineering Principles

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72 MECHANICAL ENGINEERING PRINCIPLES

given by:


M=RA×x− 6 (x− 3 )= 2. 4 x− 6 (x− 3 )

= 2. 4 x− 6 x+ 18

i.e. M= 18 − 3. 6 x(clockwise) ( 6. 3 )


The effect of this resultant moment on the left ofx
is shown in the lower diagram of Figure 6.7.


ABC

3 m 2 m

6 kN

2.4 kN 3.6 kN


x

M= 2.4x
−6 (x− 3)
= 18 − 3.6x

M= 3.6 (5 − x)
= 18 − 3.6x

Figure 6.7


Now from Figure 6.7, it can be seen that on the
right side ofx, there is an anti-clockwise moment
of:M=RB×( 5 −x)= 3. 6 ( 5 −x)= 18 − 3. 6 x


i.e. M= 18 − 3. 6 x(anti-clockwise) ( 6. 4 )


The effect of the moment of equation (6.3) and that
of the moment of equation (6.4), is to cause the
beam to sag at this point as shown by the lower
diagram of Figure 6.7, i.e.Mis positive betweenC
andB,and


M=+ 18 − 3. 6 x( 6. 5 )

Shearing force


Consider a distancexbetweenCandB, as shown
in Figure 6.8.


3 m 2 m

6 kN

F= 6 − 2.4

F= 3.6 kN

= 3.6 kN

2.4 kN 3.6 kN

x

C
AB

Figure 6.8


From Figure 6.8, it can be seen that atx, there are
two vertical forces to the left of this section, namely
the 6 kN load acting downwards and the 2.4 kN load
acting upwards, resulting in a net value of 3.6 kN
acting downwards, as shown by the lower diagram
of Figure 6.8. Similarly, by considering the vertical
forces acting on the beam to the right ofx, it can
be seen that there is one vertical force, namely the
3.6 kN load acting upwards, as shown by the lower
diagram of Figure 6.8. Thus, as the right hand of
the section is tending to slide upwards, the shearing
force is said to be negative, i.e. betweenCandB,

F=− 3 .6kN ( 6. 6 )

It should be noted that atC, there is a discontinuity
in the value of the shearing force, where over an
infinitesimal length the shearing force changes from
+ 2 .4kNto− 3 .6 kN, from left to right.

Bending moment and shearing force diagrams

The bending moment and shearing force diagrams
are simply diagrams representing the variation of
bending moment and shearing force, respectively,
along the length of the beam. In the bending moment
and shearing force diagrams, the values of the bend-
ing moments and shearing forces are plotted ver-
tically and the value ofxis plotted horizontally,
wherex=0 at the left end of the beam andx=the
whole length of the beam at its right end.
In the case of the beam of Figure 6.4, bending
moment distribution betweenAandCis given by
equation (6.1), i.e.M= 2. 4 x, where the value ofx
varies betweenAandC.
AtA,x=0, thereforeMA= 2. 4 × 0 = 0
and atC,x =3 m, thereforeMC = 2. 4 × 3 =
7 .2kN.
Additionally, as the equation M = 2. 4 x is
a straight line, the bending moment distribution
betweenAandCwill be as shown by the left side
of Figure 6.9(a).
Similarly, the expression for the variation of
bending moment betweenCandBis given by equa-
tion (6.3), i.e.M= 18 − 3. 6 x, where the value ofx
varies betweenCandB. The equation can be seen
to be a straight line betweenCandB.
AtC,x=3 m, thereforeMC= 18 − 3. 6 × 3 =
18 − 10. 8 = 7 .2kNm
AtB,x=5 m, thereforeMB= 18 − 3. 6 × 5 =
18 − 18 = 0
Therefore, plotting of the equationM= 18 − 3. 6 x
betweenC andB results in the straight line on
the right of Figure 6.9(a), i.e. the bending moment
diagram for this beam has now been drawn.
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