534 basic knowledge in strength of materials applied in marine enginee
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534
BASIC KNOWLEDGE IN STRENGTH OF MATERIALS APPLIED
IN MARINE ENGINEERING FOR MARITIME OFFICERS
Application 11.2
EQUIVALENT STRESSES IN A RECTANGULAR CROSS SECTION
We consider that the crankshaft web can be modeled as a bar having a
rectangular cross section. Tasks:
h
H
|ட
E
N
B
D
Y
F
b
Figure 11.13 - Rectangular section
and the designation of the points
where the equivalent stresses must
be computed
1. plot the diagrams of the normal stress;
2. determine the values of the equivalent
stresses in the contour points: A, B, C, D,
E, F, G, H.
Input data:
1. geometric data:
h = 18.a,
α = 0.267,
b = 6.a,
2. internal forces and moments in the
cross section where the calculus is
performed:
-160. pa
MX = +800. pa²
My = -1050. pa²
M₂ =-750-pa²
Mz
Coviedol M v2 3BN 17806630 53
Reminder of the theoretical notions
Solution
Normal stress is produced by axial forces, N, and bending moments, My
and
Mz.
σ(y, z) =
Mz
Iz
computed using Navier's relation, (10.21),
Mz
··y=σª +σ¾¢ +σ¼z, where, according to (8.1) and
Y
=
'
My (y, z) =
σr (y,z)= My.z,
Mz (y, z) =
==
A
Mz
Iz
∙y.
Iy
The neutral axis is the locus² of the points in the section where the normal
stress is null and it has the equation, (10.26): σ(y, z) =0, namely, (10.27),
N MY
+
A Iy
Mz
y= 0. The coordinates of the neutral axis intersection points
Iz
with the two axes OY, and OZ, respectively are obtained by equaling with zero
each of the coordinates, one at a time, which leads to the set of points
2 the set of all entities (points, lines or surfaces) that satisfy a given requirement FAILURE THEORIES
535
Iz N
.
YI₁
=
A Mz and
y₁₁ = 0
Drawing the neutral axis is important in order
Iy N
Z12
=
A MY
to easily identify the most remote point in the section with respect to this axis,
points where the normal stresses have extreme values.
Tangential or shear stresses are produced by the torque (MX) and by the
shear forces (Ty,Tz).
To compute the tangential stresses produced by torsion, there are specific
calculus relations for each shape of the cross section. In this case, having a
rectangular cross section, and considering that h>b, according to (9.61),
use the following calculus relations:
Mx
max max
Mx
max
M
X
=
a.h.b²
M
X
a'.h.b²
The overall maximum tangential stress □
Mx
2
max max
found at the middle
max
of the long side (of h dimension), and a local ‘maximum' tangential stress TMX is
located at the middle of the shorter side of the rectangle (of b dimension).
Coefficients a and a' are taken from the tables where are listed in respect with
h
the ratio, or are determined using some alculus relations resulted from the
b
book Son0-630 53
Theory of Elasticity. In this case coefficients a and a' are given in the problem
hypothesis, being considered as associated information to the primary geometric
data, i. e. h and b.
Tangential stresses generated by the shear forces Ty and T₂ are
computed using Juravski'
Tz Sy
by
relation, (10.68),
Ty
ST
TTY
bz
A series of geometrical characteristics appear in these relations and they
have to be computed:
1. Area of the cross section is computed by A=h·b
3
b.h³
h.b³
3
moments of area are computed using: Iy
=
'
Iz
=
These
12
12
relations can be better remembered by using the mnemonic rule I
=
axis 12
where || is the side parallel to the reference axis and _ is the side perpendicular
on the reference axis.
3. Maximum values of the first moments of area Sy and S₂ can be calculated for
half of the cross section, which has a rectangular shape. Thus, they are computed
as a product between the area of a half of section and distance from the centroid
of that given area to the axis in respect with which the first moment of area is
being computed. 536
BASIC KNOWLEDGE IN STRENGTH OF MATERIALS APPLIED
IN MARINE ENGINEERING FOR MARITIME OFFICERS
0.25-b
A=h.0.5b
0.5.h
Y
0.25-h
Y
Z
A=0.5h-b
Sy=(0.5h-b)-0.25h
0.5-b
Z
Sz=(h-0.5b)-0.25b
Figure 11.14 - Calculus scheme of the first moment
with respect to axis Y and Z
rea,
Therefore, for the rectangular cross section the first moment of area
has the maximum value in its centroid, namely for half of the section. Its
corresponding area is A
=
h
h
2
··b. The marked area
its centroid at distance
4
in respect with the horizontal axis OY. Hence, the maximum first moment of area
is Sy
=
2
hed ISBN10-00539.4
h
4
distance
=
h².b
8
Area
Similarly, for the rectangular cross section, the S₂ first moment of area
has its maximum value in its centroid, namely for a half cross section. Its
corresponding area is 4 = h. The marked area has the centroid at
b
4
distance
in respect to the vertical axis OZ. Thus, the according first moment of area is
b
Sz
=
h
b
Area
Conventions to plot stress diagrams
In case we plot free body diagrams of forces or moments, we use two
conventions, namely: the sign convention and the diagrams' drawing rules.
Similarly, to plot stresses there are two conventions: a sign convention and the
diagrams' drawing rules.
As the sign convention of forces results from the system of axes and the
running sense, similarly, the sign convention for stresses results from the sign
convention for internal forces. This way, we consider that the stresses applied on
an elementary area which generate an internal force formally positive, may be
considered formally positive.
As it has been mentioned above, the problems dealing with cross section
aspects (geometrical characteristics of the cross sections, stresses) are solved FAILURE THEORIES
537
in a system of axes in which the OZ axis is vertical pointing downwards, and the
OY axis is horizontal pointing to the right. This system of axes results if the
observer is at the left side and is looking at the cross section in the direction of
the OX axis, as in the figure below.
y
Z
P
Χ
y
For such a position of the observer, the sign convention
+ Internal Force/Moment
and moments is
-axis
'
sign = +1,
internal forces
was shown in detail in
the chapter which presents the methods to draw the free body diagrams.
Bearing in mind all the above, if for the internal forces there is the
+ Force
+ Stress
then for the stresses it results the convention
-axis
-axis
convention
In what concerns the diagram drawing rules, we start from the idea that a
positive stress has as effect the local elongation of the fibers in which it is
'applied'. From here, we may derive that, in respect with a zero line signifying the
non-deflected section, the stress diagram is drawn 'towards the exterior of the
cross section' if stresses are positive, i.e. if the fibers are elongated or ‘in tension',
respectively 'towards the interior of the cross section' if the stresses are negative,
i.e. if the fibers are compressed. These are general considerations and must be
understood in the sense that they represent a manner of thinking, a way to
logically learn the drawing rules for stress diagrams, and not to actually draw a
series of stress
in a more or less complex state of stresses.
Calculus of values of the geometrical characteristics of the cross
section
the previously mentioned calculus relations, for the given cross
section (h=18.a, b=6.a) we get the following values: A=108. a²,
Iy = 2916⋅ a², I₂ =324. aª, S₁ =243.a³, S₂ = 81. a³. 538
BASIC KNOWLEDGE IN STRENGTH OF MATERIALS APPLIED
IN MARINE ENGINEERING FOR MARITIME OFFICERS
Calculus of the normal stresses
σ
My
Mz
=
=
N
A
My
==
Iy
M
- 200 pa --1.8518º
108.a²
Iz
Z
Z=
a
-1050. pa²
•Z=
-0.36008 P
• Z
2916.a4
-750.pa²
y
324-a4
Normal stress has the equation:
P
· y = +2.3148-
148 y
α
σ(y,z) = −1.8518º −0.36008 P· z+2.3148 P
a
.
2
α
.y
To compute normal stress in the specified points, we have to replace their
coordinates in the expressions above. Therefore, we have to determine the
points' coordinates.
-60639.4
A
Point A is placed on the OZ axis, therefore y₁ = 0. It is placed at the upper
extremity of the cross section, hence in the negative range of axis OZ, therefore
18.a
2
=-9.a. Consequently, point
h
ZA
2
A
A (y₁ = 0, ZA
=
= −9.a).
the
coordinates
Point B is placed in the upper right corner, thus in the quadrant of the
system of axes in which the y coordinate is positive and the z coordinate is
negative. We compute the coordinates for point B and we get
Ув = +
b
2
= +
6.a
2
= +3.a and
ZB
18.a
2
=-9.a. Hence, point B has the
.
coordinates B (y B = +3 · α, ZB
Point C is placed on the OY axis, hence zc = 0. It is placed at the right
extremity of the cross section, hence in the positive range of the OY axis,
b
therefore yc= =+==
C(y = +3.a, zc
= +3. a. Therefore, point C has the coordinates
Point D is placed in the lower right corner thus in the quadrant in which
both coordinates are positive. We calculate the coordinate of point D and we get
YD = +
6.a
2
h
18.a
= +3.a and Z₁ = +
= +
2
=+9·a. Thus, point D has the
2
coordinates D (y₁ = +3⋅a, z₁ = +9⋅a).
D
Point E is placed on the OZ axis, therefore yĘ = 0. It is placed at the lower
extremity of the cross section, hence in the positive range of the OZ axis, hence
h
18.a
= =+==+
2
= +9.a.
2
ZE
=
+9⋅ a).
E (YE = 0,
Therefore,
point E has
the
coordinates
Point F is placed in the lower left corner, therefore in the quadrant in which
the y coordinate is negative and the z coordinate is positive. We compute the
b
6.a
coordinate of point F and
we
get YF
=-3.a and
2
2