2542x_appa
Transcript of 2542x_appa
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799
Appendix
AProperties of a Plane Area
Because of their importance in connection with the analysis of bending
and torsion, certain relations for the second-area moments, commonly
referred to as moments of inertia, are indicated in the following
paragraphs. The equations given are in reference to Fig. A.1, and
the notation is as follows:
A area of the section
X ;Y rectangular axes in the plane of the section at arbitrary pointO
x; y rectangular axes in the plane of the section parallel to X ;Y ;respectively with origin at the centroid, C, of the section
Figure A.1 Plane area.
-
z polar axis through C
x0; y0 rectangular axes in the plane of the section, with origin at C,inclined at a counterclockwise angle y from x; y
1, 2 principal axes at C inclined at a counterclockwise angle ypfrom x; y
r the distance from C to the dA element, r x2 y2
pBy definition,
Moments of inertia: Ix A
y2 dA; Iy A
x2 dA
Polar moment of inertia:
Iz J A
r2 dA Ix Iy Ix0 Iy0 I1 I2Product of inertia: Ixy
A
xy dA
Radii of gyration: kx Ix=A
p; ky
Iy=A
pParallel axis theorem:
IX Ix Ay2c ; IY Iy Ax2c ; IXY Ixy AxcycTransformation equations:
Ix0 Ix cos2 y Iy sin2 y Ixy sin 2yIy0 Ix sin2 y Iy cos2 y Ixy sin 2yIx0y0 12 Ix Iy sin 2y Ixy cos 2y
Principal moments of inertia and directions:
I1;2 12 Ix Iy Iy Ix2 4I2xy
q ; I12 0;
yp 12 tan12Ixy
Iy Ix
!
Upon the determination of the two principal moments of inertia, I1and I2, two angles, 90
apart, can be solved for from the equation for yp.It may be obvious which angle corresponds to which principal moment
of inertia. If not, one of the angles must be substituted into the
equations Ix0 and Iy0 which will again yield the principal moments of
inertia but also their orientation.
Note, if either one of the xy axes is an axis of symmetry, Ixy 0; withIx and Iy being the principal moments of inertia of the section.
If I1 I2 for a set of principal axes through a point, it follows thatthe moments of inertia for all x0y0 axes through that point, in the sameplane, are equal and Ix0y0 0 regardless of y: Thus the moment ofinertia of a square, an equilateral triangle, or any section having
800 Formulas for Stress and Strain [APP. A
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two or more axes of identical symmetry is the same for any central
axis.
The moment of inertia and radius of gyration of a section with
respect to a centroidal axis are less than for any other axis parallel
thereto.
The moment of inertia of a composite section (one regarded as made
up of rectangles, triangles, circular segments, etc.) about an axis is
equal to the sum of the moments of inertia of each component part
about that axis. Voids are taken into account by subtracting the
moment of inertia of the void area.
Expressions for the area, distances of centroids from edges,
moments of inertia, and radii of gyration are given in Table A.1 for a
number of representative sections. The moments of products of inertia
for composite areas can be found by addition; the centroids of compo-
site areas can be found by using the relation that the statical moment
about any line of the entire area is equal to the sum of the statical
moments of its component parts.
Although properties of structural sectionswide-flange beams,
channels, angles, etc.are given in structural handbooks, formulas
are included in Table A.1 for similar sections. These are applicable to
sections having a wider range of web and flange thicknesses than
normally found in the rolled or extruded sections included in the
handbooks.
Plastic or ultimate strength design is discussed in Secs. 8.15 and
8.16, and the use of this technique requires the value of the fully
plastic bending momentthe product of the yield strength of a ductile
material and the plastic section modulus Z. The last column in Table
A.1 gives for many of the sections the value or an expression for Z and
the location of the neutral axis under fully plastic pure bending. This
neutral axis does not, in general, pass through the centroid,
but instead divides the section into equal areas in tension and
compression.
APP. A ] Properties of a Plane Area 801
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TABLE A.1 Properties of sectionsNOTATION: A area length2; y distance to extreme fiber (length); I moment of inertia length4; r radius of gyration (length); Z plastic section modulus length3; SF shape factor. SeeSec. 8.15 for applications of Z and SF
Form of section
Area and distances from
centroid to extremities
Moments and products of inertia
and radii of gyration about central axes
Plastic section moduli,
shape factors, and locations
of plastic neutral axes
1. Square A a2
yc xc a
2
y0c 0:707a cosp4 a
Ix Iy I 0x 112 a4
rx ry r0x 0:2887aZx Zy 0:25a3
SFx SFy 1:5
2. Rectangle A bd
yc d
2
xc b
2
Ix 112 bd3
Iy 112 db3
Ix > Iy if d > b
rx 0:2887dry 0:2887b
Zx 0:25bd2
Zy 0:25db2
SFx SFy 1:5
3. Hollow rectangle A bd bidi
yc d
2
xc b
2
Ix bd3 bid3i
12
Iy db3 dib3i
12
rx IxA
1=2
ry Iy
A
1=2
Zx bd2 bid2i
4
SFx Zxd
2Ix
Zx db2 dib2i
4
SFy Zyb
2Iy
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4. Tee section A tb twd
yc bt2 twd2t d
2tb twd
xc b
2
Ix b
3d t3 d
3
3b tw Ad t yc2
Iy tb3
12 dt
3w
12
rx IxA
1=2
ry Iy
A
1=2
If twd5 bt, then
Zx d2tw
4 b
2t2
4tw btd t
2
Neutral axis x is located a distance bt=tw d=2from the bottom.
If twd4 bt, then
Zx t2b
4 twdt d twd=2b
2
Neutral axis x is located a distance twd=b t=2from the top.
SFx Zxd t yc
I1
Zy b2t t2wd
4
SFy Zyb
2Iy
5. Channel section A tb 2twd
yc bt2 2twd2t d
2tb 2twd
xc b
2
Ix b
3d t3 d
3
3b 2tw Ad t yc2
Iy d tb3
12 db 2tw
3
12
rx IxA
1=2
ry Iy
A
1=2
If 2twd5 bt, then
Zx d2tw
2 b
2t2
8tw btd t
2
Neutral axis x is located a distance
bt=2tw d=2 from the bottom.If 2twd4 bt, then
Zx t2b
4 twd t d
twd
b
Neutral axis x is located a distance twd=b t=2from the top.
SFx Zxd t yc
Ix
Zy b2t
4 twdb tw
SFy Zyb
2Iy
APP.A]
Propertie
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TABLE A.1 Properties of sections (Continued)
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TABLE A.1 Properties of sections (Continued)
Form of section
Area and distances from
centroid to extremities
Moments and products of inertia
and radii of gyration about central axes
Plastic section moduli,
shape factors, and locations
of plastic neutral axes
6. Wide-flange beam with
equal flanges
A 2bt twd
yc d
2 t
xc b
2
Ix bd 2t3
12 b twd
3
12
Iy b3t
6 t
3wd
12
rx IxA
1=2
ry Iy
A
1=2
Zx twd
2
4 btd t
SFx Zx yc
Ix
Zy b2t
2 t
2wd
4
SFy Zyxc
Iy
7. Equal-legged angle A t2a t
yc1 0:7071a2 at t2
2a t
yc2 0:7071a2
2a txc 0:7071a
Ix a4 b4
12 0:5ta
2b2
a b
Iy a4 b4
12where b a t
rx IxA
1=2
ry Iy
A
1=2
Let yp be the vertical distance from the top corner to
the plastic neutral axis. If t=a5 0:40, then
yp at
a t=a
2
2
" #1=2
Zx Ayc1 0:6667ypIf t=a4 0:4, then
yp 0:3536a 1:5tZx Ayc1 2:8284y2pt 1:8856t3
8. Unequal-legged angle A tb d t
xc b2 dt t22b d t
yc d2 bt t22b d t
Ix 13 bd3 b td t3 Ad yc2
Iy 13 db3 d tb t3 Ab xc2
Ixy 14 b2d2 b t2d t2 Ab xcd yc
rx IxA
1=2
ry Iy
A
1=2
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9. Equilateral triangle A 0:4330a2
yc 0:5774axc 0:5000ay0c 0:5774a cos a
Ix Iy Ix0 0:01804a4
rx ry rx0 0:2041aZx 0:0732a3; Zy 0:0722a3
SFx 2:343; SFy 2:000Neutral axis x is 0:2537a from the base.
10. Isosceles triangle A bd2
yc 23 d
xc b
2
Ix 136 bd3
Iy 148 db3
Ix > Iy if d > 0:866b
rx 0:2357dry 0:2041b
Zx 0:097bd2; Zy 0:0833db2
SFx 2:343; SFy 2:000Neutral axis x is 0:2929d from the base.
11. Triangle A bd2
yc 23 dxc 23 b 13 a
Ix 136 bd3
Iy 136 bdb2 ab a2Ixy 172 bd2b 2a
yx 1
2tan1
db 2ab2 ab a2 d2
rx 0:2357d
ry 0:2357b2 ab a2
p
12. Parallelogram A bd
yc d
2
xc 12 b a
Ix 112 bd3
Iy 112 bdb2 a2Ixy 112 abd2
yx 1
2tan1
2adb2 a2 d2
rx 0:2887d
ry 0:2887b2 a2
p
APP.A]
Propertie
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TABLE A.1 Properties of sections (Continued)
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TABLE A.1 Properties of sections (Continued)
Form of section
Area and distances from
centroid to extremities
Moments and products of inertia
and radii of gyration about central axes
Plastic section moduli,
shape factors, and locations
of plastic neutral axes
13. Diamond A bd2
yc d
2
xc b
2
Ix 148 bd3
Iy 148 db3
rx 0:2041dry 0:2041b
Zx 0:0833bd2; Zy 0:0833db2
SFx SFy 2:000
14. Trapezoid A d2b c
yc d
3
2b cb c
xc 2b2 2bc ab 2ac c2
3b c
Ix d3
36
b2 4bc c2b c
Iy d
36b c b4 c4 2bcb2 c2
ab3 3b2c 3bc2 c3 a2b2 4bc c2
Ixy d2
72b c c3b2 3bc c2
b3 a2b2 8bc 2c2
15. Solid circle A pR2
yc RIx Iy
p4
R4
rx ry R
2
Zx Zy 1:333R3
SFx 1:698
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16. Hollow circle A pR2 R2i yc R
Ix Iy p4R4 R4i
rx ry 12R2 R2i
qZx Zy 1:333R3 R3i
SFx 1:698R4 R3i RR4 R4i
17. Very thin annulus A 2pRtyc R
Ix Iy pR3trx ry 0:707R
Zx Zy 4R2t
SFx SFy 4
p
18. Sector of solid circle A aR2
yc1 R 1 2 sin a
3a
yc2 2R sin a
3a
xc R sin a
Ix R4
4a sin a cos a 16 sin
2 a9a
!
Iy R4
4a sin a cos a
Note: If a is small; a sin a cos a 23a3 2
15a5
rx R
2
1 sin a cos a
a 16 sin
2 a9a2
s
ry R
2
1 sin a cos a
a
r
If a4 54:3, then
Zx 0:6667R3 sin aa3
2 tan a
1=2" #
Neutral axis x is located a distance
R0:5a= tan a1=2 from the vertex.If a5 54:3, then
Zx 0:6667R32 sin3 a1 sin a where theexpression 2a1 sin 2a1 a is solved for the valueof a1.Neutral axis x is located a distance R cos a1 fromthe vertex.
If a4 73:09, then SFx Zxyc2
Ix
If 73:094a4 90, then SFx Zxyc1
Ix
Zy 0:6667R31 cos aIf a4 90 , then
SFy 2:6667 sin a1 cos a
a sin a cos aIf a5 90 , then
SFy 2:66671 cos a
a sin a cos a
APP.A]
Propertie
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TABLE A.1 Properties of sections (Continued)
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TABLE A.1 Properties of sections (Continued)
Form of section
Area and distances from
centroid to extremities
Moments and products of inertia
and radii of gyration about central axes
Plastic section moduli,
shape factors, and locations
of plastic neutral axes
19. Segment of solid circle
(Note: If a4p=4, useexpressions from case 20)
A R2a sin a cos a
yc1 R 1 2 sin
3 a3a sin a cos a
" #
yc2 R2 sin
3 a3a sin a cos a cos a" #
xc R sin a
Ix R4
4a sin a cos a 2 sin3 a cos a 16 sin
6 a9a sin a cos a
" #
Iy R4
123a 3 sin a cos a 2 sin3 a cos a
rx R
2
1 2 sin
3 a cos aa sin a cos a
16 sin6 a
9a sin a cos a2
s
ry R
2
1 2 sin
3 a cos a3a sin a cos a
s
20. Segment of solid circle
(Note: Do not use if
a > p=4
A 23R2a31 0:2a2 0:019a4
yc1 0:3Ra21 0:0976a2 0:0028a4yc2 0:2Ra21 0:0619a2 0:0027a4xc Ra1 0:1667a2 0:0083a4
Ix 0:01143R4a71 0:3491a2 0:0450a4Iy 0:1333R4a51 0:4762a2 0:1111a4rx 0:1309Ra21 0:0745a2ry 0:4472Ra1 0:1381a2 0:0184a4
21. Sector of hollow circle A at2R t
yc1 R 1 2 sin a
3a1 t
R 1
2 t=R
yc2 R2 sin a
3a2 t=R 1 t
R
2 sin a 3a cos a
3a
xc R sin a
Ix R3t 1 3t
2R t
2
R2 t
3
4R3
a sin a cos a 2 sin2 a
a
!
t2 sin
2 a3R2a2 t=R 1
t
R t
2
6R2
#
Iy R3t 1 3t
2R t
2
R2 t
3
4R3
a sin a cos a
rx IxA
r; ry
Iy
A
r(Note: If t=R is small, a canexceed p to form anoverlapped annulus)
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Note: If a is small:sin aa
1 a2
6 a
4
120; a sin a cos a 2
3a3 1 a
2
5 2a
4
105
;
sin2 aa
a 1 a2
3 2a
4
45
cos 1 a2
2 a
4
24; a sin a cos a 2 sin
2 aa
2a5
451 a
2
7 a
4
105
22. Solid semicircle A p2
R2
yc1 0:5756Ryc2 0:4244Rxc R
Ix 0:1098R4
Iy p8
R4
rx 0:2643R
ry R
2
Zx 0:3540R3; Zy 0:6667R3
SFx 1:856; SFy 1:698Plastic neutral axis x is located a distance 0:4040R
from the base.
23. Hollow semicircle
Note: b R Ri2
t R Ri
A p2R2 R2i
yc2 4
3pR3 R2iR2 R2i
or
yc2 2b
p1 t=b
2
12
" #
yc1 R yc2xc R
Ix p8R4 R4i
8
9pR3 R3i 2
R2 R2ior
Ix 0:2976tb3 0:1805bt3 0:00884t5
b
Iy p8R4 R4i
or
Iy 1:5708b3t 0:3927bt3
Let yp be the vertical distance from the bottom to the
plastic neutral axis.
yp 0:7071 0:2716C 0:4299C2 0:3983C3RZx 0:8284 0:9140C 0:7245C2
0:2850C3R2twhere C t=RZy 0:6667R3 R3i
24. Solid ellipse A pabyc axc b
Ix p4
ba3
Iy p4
ab3
rx a
2
ry b
2
Zx 1:333a2b; Zy 1:333b2aSFx SFy 1:698
APP.A]
Propertie
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TABLE A.1 Properties of sections (Continued)
-
TABLE A.1 Properties of sections (Continued)
Form of section
Area and distances from
centroid to extremities
Moments and products of inertia
and radii of gyration about central axes
Plastic section moduli,
shape factors, and locations
of plastic neutral axes
25. Hollow ellipse A pab aibiyc axc b
Ix p4ba3 bia3i
Iy p4ab3 aib3i
rx 1
2
ba3 bia3iab aibi
s
ry 1
2
ab3 aib3iab aibi
s
Zx 1:333a2b a2i biZy 1:333b2a b2i ai
SFx 1:698a3b a2i biaa3b a3i bi
SFy 1:698b3a b2i aibb3a b3i ai
Note: For this case the inner and outer perimeters are both ellipses and the wall
thickness is not constant. For a cross section with a constant wall thickness see
case 26.
26. Hollow ellipse with
constant wall thickness t.
The midthickness
perimeter is an ellipse
(shown dashed).
0:2 < a=b < 5
A pta b 1 K1a ba b 2" #
where
K1 0:2464 0:002222a
b b
a
yc a t
2
xc b t
2
Ix p4
ta2a 3b 1 K2a ba b 2" #
p16
t33a b 1 K3a ba b 2" #
where
K2 0:1349 0:1279a
b 0:01284 a
b
2
K3 0:1349 0:1279b
a 0:01284 b
a
2For Iy interchange a and b in the expressions
for Ix;K2, and K3
Zx 1:3333taa 2b 1 K4a ba b 2" #
t3
3
where
K4 0:1835 0:895a
b 0:00978 a
b
2For Zy interchange a and b in the expression for Zxand K4.
See the note on maximum
wall thickness in case 27.
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27. Hollow semiellipse with
constant wall thickness t.
The midthickness
perimeter is an ellipse
(shown dashed).
0:2 < a=b < 5
Note: There is a limit on the
maximum wall thickness
allowed in this case. Cusps
will form in the perimeter at
the ends of the major axis
if this maximum is exceeded.
Ifa
b4 1; then tmax
2a2
b
Ifa
b5 1; then tmax
2b2
a
A p2
ta b 1 K1a ba b 2" #
where
K1 0:2464 0:002222a
b b
a
yc2 2a
pK2
t2
6paK3
where
K2 1 0:3314C 0:0136C2 0:1097C3
K3 1 0:9929C 0:2287C2 0:2193C3
Using C a ba b
yc1 a t
2 yc2
xc b t
2
IX p8
ta2a 3b 1 K4a ba b 2" #
p32
t33a b 1 K5a ba b 2" #
where
K4 0:1349 0:1279a
b 0:01284 a
b
2
K5 0:1349 0:1279b
a 0:01284 b
a
2
Ix IX Ay2c2
For Iy use one-half the value for Iy in case 26.
Let yp be the vertical distance from the bottom to the
plastic neutral axis.
yp C1 C2a=b
C3a=b2 C4
a=b3
a
where if 0:25 < a=b4 1, then
C1 0:5067 0:5588D 1:3820D2
C2 0:3731 0:1938D 1:4078D2
C3 0:1400 0:0179D 0:4885D2
C4 0:0170 0:0079D 0:0565D2or if 14a=b < 4, then
C1 0:4829 0:0725D 0:1815D2
C2 0:1957 0:6608D 1:4222D2
C3 0:0203 1:8999D 3:4356D2
C4 0:0578 1:6666D 2:6012D2where D t=tmax and where 0:2 < D4 1
Zx C5 C6a=b
C7a=b2 C8
a=b3
4a2t
where if 0:25 < a=b4 1, then
C5 0:0292 0:3749D1=2 0:0578DC6 0:3674 0:8531D1=2 0:3882DC7 0:1218 0:3563D1=2 0:1803DC8 0:0154 0:0448D1=2 0:0233D
or if 14a=b < 4, thenC5 0:2241 0:3922D1=2 0:2960DC6 0:6637 2:7357D1=2 2:0482DC7 1:5211 5:3864D1=2 3:9286DC8 0:8498 2:8763D1=2 1:8874D
For Zy use one-half the value for Zy in case 26.
APP.A]
Propertie
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TABLE A.1 Properties of sections (Continued)
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TABLE A.1 Properties of sections Continued)
Form of section
Area and distances from
centroid to extremities
Moments and products of inertia
and radii of gyration about central axes
Plastic section moduli,
shape factors, and locations
of plastic neutral axes
28. Regular polygon with n
sidesA a
2n
4 tan a
r1 a
2 sin a
r2 a
2 tan a
If n is odd
y1 y2 r1 cos an 1
2
p
2
If n=2 is odd
y1 r1; y2 r2If n=2 is even
y1 r2; y2 r1
I1 I2 124 A6r21 a2
r1 r2 1246r21 a2
q For n 3, see case 9. For n 4, see cases 1 and 13.For n 5, Z1 Z2 0:8825r31. For an axis perpen-dicular to axis 1, Z 0:8838r31. The location of this
axis is 0.7007a from that side which is perpendicular
to axis 1. For n56, use the following expression for aneutral axis of any inclination:
Z r31 1:333 13:9081
n
2 12:528 1
n
3" #
29. Hollow regular polygon
with n sidesA nat 1 t tan a
a
r1 a
2 sin a
r2 a
2 tan a
If n is odd
y1 y2 r1 cos an 1
2 p
2
If n=2 is odd
y1 r1; y2 r2If n=2 is even
y1 r2; y2 r1
I1 I2 na3t
8
1
3 1
tan2 a
1 3 t tan aa
4 t tan aa
22 t tan a
a
3" #
r1 r2 a8
p
1
3
1
tan2 a1 2 t tan a
a 2 t tan a
a
2" #vuut
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Table of ContentsAppendix A: Properties of a Plane AreaAppendix B:Glossary: DefinationsAppendix C: Composite Materials