plat baja
DESCRIPTION
strukturTRANSCRIPT
-
CONTINUOUS INFLUENCE LINES F O R . SPAN MOMENTS.
BEAM OVER INFINITE NUMBER OF ELASTIC SUPPORTS.
APPENDIX C
8
i 7 6
I i
5
*r- -
4
I
' 3
J
2
>
1
0
1
0
m
1
_
2
3
e
4
I
in
t
6
t \
7 8 J
ORDINATES FOR BENDING
T MOMENT j - AT SECTION m - m DUE TO A LOAD P = l AT ANY ARBITRARY SUPPORT.
tf 0 8
OO
0.02 0 .04 0 .06 0.08
+ 0 .01321 + 0 .02313 + 0 .03130 + 0 .03839
- 0.01465 - 0. 02333 - 0.02917 - 0. 03344
+ 0. 00125 - 0 . 0 0 0 8 7 - 0 . 0 0 3 8 3 - 0 .00700
+ 0.00024 + 0 .00102 + 0 .00150 + 0 .00149
- 0 .00006 0. 00004 + 0. 00029 + 0. 00068
0 0.00004 0.00010 0.00002
+ 0.00001 - 0 . 0 0 0 0 5
0 0. 00001
0. 1 0. 2 0. 3 0. 4
+ 0.04468 + 0 .06902 + 0.08713 + 0. 10188
0.03674 0 .04 538 0. 04835 0. 04 903
0. 01015 0. 01628 0.03450 0. 04268
+ 0 .00122 + 0 .00495 - 0 . 0 0 8 1 6 - 0 .0 1384
+ 0. 00 155 + 0.00198 + 0. 00 148 + 0. 00005
+ 0.00009 + 0.00100 + 0.00187 + 0.00237
- 0.00007 + 0.00010 + 0.00062 + 0.00122
- 0 .00002 - 0 .00009
0 + 0 .00023
0 0. 00004 0.00010 0. 00010
0. 5 0 .6 0. 7 0.8 0 .9
+ 0. 11450 + 0. 12559 + 0. 13555 + 0. 14459 + 0. 15297
0.04858 0.04 743 0.04591 0.04417 0.04 198
0. 04932 0.05473 0.05593 0 .06311 0. 06640
- 0.01935 - 0. 02454 - 0.0294 1 - 0 .03395 - 0 .03819
- 0 . 00196 - 0.00428 - 0.00681 - 0.00943 - 0 . 0121 -
+ 0.00248 + 0 .00226 + 0. 00 1 78 + 0.00107 + 0.00019
+ 0.00180 + 0 .00227 + 0.00262 + 0.00286 + 0 .00297
+ 0.00057 + 0.00096 + 0.00136 + 0.00175 + 0.00211
- 0. 00002 + 0. 00023 + 0.00034 + 0 .00052 + 0. 000 77
1. 0 1. 5 2 .0 3. 0 4. 0
+ 0. 16073 + 0. 19322 + 0. 21895 + 0. 25930 + 0. 29104
- 0.04018 - 0. 02944 - 0. 01876 + 0. 00 107 + 0.01881
0. 06923 0. 07881 0. 08383 0. 08 748 0. 08705
0.04216 0.05860 0. 07094 0 .08821 0.09957
0.01478 0 .02771 0.03933 0.05869 0. 07298
0.00080 0. 00715 0.01436 0.0288 1 0. 04215
+ 0.00297 + 0.00166 - 0.00115 - 0. 00889 - 0 .01764
+ 0.00242 + 0 .00340 + 0 .00333 + 0.00092 - 0 . 0 0 3 2 8
+ 0. 001 10 + 0 .00243 + 0. 00340 + 0. 00396 + 0 .00300
5. 0 6. 0 7.0 8. 0 9. 0 10.0
+ 0. + 0 + 0. + 0. + 0
31756 34052 36139 37926 39604
+ 0. 41 154
+ 0. 03484 + 0 .04947 + 0 .06347 + 0 .07552 + O. 08728 + 0 . 098 3 5
0. 08469 0. 08 130 0.07733 0. 07302 0. 06855 0. 06394
0. 10751 0. 1 1315 0. 11722 0. 12014 0. 12221 O. 12362
0. 08641 0. 09665 0. 10526 0. 11257 0. 11855 0. 12430
0.05413 0.0648 5 0.07448 0.08317 0.09103 O.09820
- 0 .02651 - 0.03512 - 0.04335 - 0. 05117 - 0.05856 - 0. 06555
- 0. 00839 - 0. 01395 - 0. 01970 - 0 .02549 - 0 .03123 _ O. 03 688
0. 00099 0.00174 0. 00497 0 .00849 0.01223 O. O1610
TABLE 2 INFLUENCE LINES FOR SUPPORT MOMENTS.
CONTINUOUS BEAM OVER INFINITE NUMBER OF ELASTIC SUPPORTS.
APPENDIX C
-
to CO
0* 0. 02 0. 04 0 .06 0. 08
0. 1 0. 2 0. 3 0. 4
0. 5 0. 6 0. 7 0. 3 0. 9
1. 0 1. 5 2. 0 3. 0 4 .0
5. 0 6. 0 7. 0 8. 0 9.0
10. 0
TABLE 2 INFLUENCE LINES FOF
CONTINUOUS BEAM OVER INFINITE
Tff
3 8 7 6 5 4 3 2 1 0
t ^ ^ ^ ^ ^ ^ ^ X . 1 . e E i. |. 1 . I * C ?
ORDINATES FOR BENDING MOMENT -M_ AT SUPPORT 0 I
0 + 0.05763 + 0.08919 + 0.11111 + 0. 12800
+ 0. 14183 + 0. 18859 + 0.21870 + 0.24142
+ 0. 25989 + 0.27556 + 0. 28924 + 0. 30143 + 0. 31245
+ 0. 32254 + 0.36346 + 0. 394 70 + 0.44218 + 0.47857
+ 0. 50847 + 0. 53406, + 0.55656 + 0. 57672 + 0. 59502 + 0.61185
I - 0 .03121 - 0.04294 - 0 .04850 - 0.05128
- 0. 05257 - 0 .05056 - 0 .04445 - 0. 03 766
- 0 .03090 - 0.02438 - 0 .01814 - 0 .01225 - 0 .00651
- 0. 00108 + 0 .02297 + 0 .04319 + 0.07641 + 0. 10351
+ 0. 12664 + 0. 14698 + 0. 16522 + 0 . 18180 + 0. 19706 + C .21122
2 + 0 .00191 - 0 .00361 - 0 . 0 0 9 8 5 - 0 . 0 1 5 6 6
- 0. 02091 - 0 .04019 - 0.05224 - 0 .06040
- 0. 06625 - 0 .07049 - 0 .07368 - 0 .07609 - 0. 07791
- 0 .07927 - 0.08184 - 0 .08071 - 0.07428 - 0.06588
- 0 .05697 - 0.04804 - 0 .03927 - 0.03075 - 0 .02250
0.01452
3 + 0 .00060 + 0 .00187 + 0 .00219 + 0 .00166
+ 0 .00061 - 0 . 0 0 7 6 4 - 0 .01665 - 0 .02496
- 0 .03238 - 0 .03897 - 0 .04486 - 0 .05013 - 0 .05489
- 0 .05919 - 0 .07577 - 0 .08695 - 0. 10068 - 0. 10822
- 0. 11241 - 0. 11456 - 0 .11538 - 0 .11529 - 0. 11456
0. 11335
4 - 0. 00011 + 0. 00017 + 0. 00080 + 0.00133
+ 0.00182 + 0.00226 + 0.00034 - 0 . 0 0 2 7 2
- 0.00631 - 0.01010 - 0.01395 - 0.01776 - 0. 02149
- 0.02512 - 0.04142 - 0.05492 - 0.07573 - 0.09092
- 0. 10261 - 0. 11174 - 0. 11905 - 0. 12499 - 0. 12986 - ) . 13389
SUPPORT NUMBER OF
1 2
k. 4 i I
MOMENTS. ELASTIC
3 4
x k \ I
SUPPORTS.
5 6
/rfff frf/f
*
DUE TO A LOAD P = |
5 0
- 0 .00009 - 0. 00023 + 0. 00004
+ 0 .00027 + 0 .00170 + 0 .00262 + 0 .00281
+ 0 .00240 + 0.00154 + 0 .00034 - 0 .00109 - 0 .00271
- 0. 00444 - 0 .01399 - 0 .02373 - 0 .04165 - 0. 05704
- 0 .07021 - 0 .08156 - 0 .09146 - 0. 10015 - 0. 10785
0. 11471
6
0 + 0 .00003 - 0 . 0 0 0 0 9
- 0 .00010 - 0 . 0 0 0 3 1 + 0 .00112 + . 0 .00192
+ 0 .00256 + 0 .00298 + 0 .00321 + 0 .00323 + 0 .00309
+ 0 .00280 - 0 . 0 0 0 3 1 - 0 . 0 0 4 9 8 - 0 . 0 1 5 9 6 - 0 .02726
- 0 .03805 - 0 .04814
' - 0 .05751 - 0 .06618 - 0 .07422
0.08168
I
APl'ENUDC C
7 8 9 X X X
I e I
AT ANY ARBITRARY SUPPORT.
7
0 - 0. 00002
- 0. 00004 - 0 .00010 + 0 .00011 + 0. 00052
+ 0. 00103 + 0 .00155 + 0 .00203 + 0 .00249 + 0 .00286
+ 0. 00314 + 0 .00363 + 0. 00268 - 0 . 0 0 1 8 1 - 0 . 0 0 8 0 3
- 0 .01496 - 0. 02209 - 0. 02920 - 0 .03616 - 0 .04291
0 .04941
8
0
0 - 0 .00007 - 0 .00012 - 0 .00006
+ 0 .00011 + 0.00037 + 0.00068 + 0.00100 + 0.00135
+ 0 .00169 + 0.00317 + 0 .00397 + 0.00364 + 0.00148
- 0 .00182 - 0. 00580 - 0 .01019 - 0 .01482 - 0 .01956
0.02434
9
0 - 0 .00001 - 0. 00008 - 0.00013
- 0.00014 - 0. 00008
+ 0.00014 + 0-. 0003 1
+ 0 .00050 + 0.00168 + 0.00283 + 0.00428 + 0.00453
+ 0 .00379 + 0 .00231 + 0.00025 - 0 . 0 0 2 1 7 - 0 . 0 0 4 90 - ( J.007B5
-
U l _ l _ _
CONTINUOUS
6 5 4
INFLUENCE LINES FOR REACTIONS BEAM OVER INFINITE NUMBER OF ELASTIC SUPPORTS.
3 2 I O I 2 3 4 5 6
APl'KNDIX C
I X I I
T T+.
i 7T T7l
I TT- yTftr 7*^9 T&
I I I > J
I -rr rT^
I -rr ~r*
I 7 T Tr~
I TT TTJ
I -rr T f
I -rr -rrt
I rr *?
1 I J
I
ORDINATES FOR REACTION AT SUPPORT Q DUE TO A LOAD P = | AT ANY ARBITRARY SUPPORT.
t 0 8 0. 02 0.04 0.06 0. 08
+ 0 . 8 2 2 3 2 + 0. 73571 * 0 . 68078 + 0. 6 4 1 4 4
+ 0 . 12196 * 0 . 17146 + 0 . 19826 + 0 . 2 1490
0. 0 3 4 4 3 0. 0 3 3 8 5 0. 0 2 6 6 1 0 . 0 1 8 3 0
+ 0.00060 - 0 . 0 0 7 1 8 - 0 . 0 1 3 4 3 - 0 . 0 1 7 6 5
+ 0 . 0 0 0 8 2 + 0 . 0 0 1 4 4 + 0 . 0 0 0 3 6 - 0 . 0 0 0 9 6
- 0. 00011 + 0. 0 0 0 3 5 + 0 . 0 0 1 2 9 + 0. 0 0 1 1 6
- 0.00009 - 0.00029 + 0. 00020
+ 0.00003 -0.00005
0 0
- 0.00002
0. 1 0. 2 0. 3 0.4
+ 0. 61 120 + 0 . 5 2 1 7 0 + 0 . 4 7 3 6 8 + 0 . 4 4 1 8 3
+ 0 . 2 2 6 0 6 + 0 . 2 4 9 5 1 + 0 . 2 5 5 3 7 + 0 . 2 5 6 3 4
- 0 . 0 1 0 1 3 + 0 . 0 2 2 1 9 + 0 . 0 4 3 3 7 + 0 . 0 5 8 1 9
- 0 . 0 2 0 3 2 - 0 . 0 2 2 6 6 - 0 . 0 1 8 5 3 - 0 . 0 1 3 2 1
0 . 0 0 2 7 6 0 . 0 1 0 4 6 0 . 0 1 4 7 1 0 . 0 1 6 7 0
+ 0. 001 18 - 0 . 0 0 0 8 3 - 0. 00379 - 0. 0 0 6 4 2
+ 0 . 0 0 0 4 3 + 0 . 0 0 0 9 8 + 0 . 0 0 0 5 0 - 0 . 0 0 0 5 0
- 0. 00002 + 0.00044 + 0.00078 + 0.00082
- 0 . 0 0 0 0 4 + 0 . 0 0 0 0 3 + 0. 0 0 0 2 7 + 0 . 0 0 0 5 1
0. 5 0. 6 0. 7 0 . 8 0 . 9
+ 0 . 4 1 8 4 2 + 0 . 4 0 0 1 3 + 0. 3 8 5 2 4 + 0 . 3 7 2 6 4 + 0 . 362C3
+ 0 . 0 2 5 5 5 + 0 . 2 5 3 8 2 + 0 . 2 5 1 8 4 + 0 . 2 4 9 9 8 + 0 . 2 4 7 5 6
+ 0 + 0. + 0 + 0 + 0.
06916 07763 08436 08980 09443
- 0 . 0 0 7 7 7 - 0. 0 0 2 6 5 + 0 . 0 2 0 9 0 + 0 . 0 0 6 4 1 + 0 . 0 1 0 3 8
0. 0 1 7 3 6 0 . 0 1 7 2 3 0. 0 1 6 6 2 0 . 0 1 5 7 1 0 . 0 1 4 6 2
0. 0 0 8 5 5 0. 0 1 0 1 9 0 . 0 1 1 0 8 0. 0 1 2 3 5 0. 0 1298
- 0.00169 - 0.00288 - 0.00405 - 0. 0 0 5 0 6 - 0. 0 0 6 0 2
+ 0 . 0 0 0 6 0 + 0 . 0 0 0 2 5 - 0 . 0 0 0 1 7 - 0 . 0 0 0 7 5 - 0 . 0 0 1 2 9
+ 0.00067 + 0.00074 + 0.00067 + 0.00062 + 0.00047
1. 0 1. 5 2 . 0 3. 0 4. 0
+ 0.35276 + 0. 31901 + 0.29700 + 0. 26847 + 0.24988
+ 0 . 2 4 5 4 3 + 0 . 2 3 5 6 9 + 0 . 2 2 7 6 0 + 0 . 2 1 5 0 7 + 0 . 2 0 5 6 8
+ 0 . 0 9 8 2 7 + 0 . 11087 + 0 . 11766 + 0 . 12430 + 0 . 12705
+ 0 . 0 1400 + 0 . 0 2 8 2 9 + 0 . 0 3 8 2 6 + 0 . 0 5 1 3 5 + 0 . 0 5 9 6 4
- 0. 01340 - 0 . 0 0 6 9 2 - 0 . 0 0 0 8 4 + 0. 0 0 9 1 2 + 0 . 0 1 6 5 7
- 0. 0 1 3 4 4 - 0. 0 1 3 7 5 - 0. 01243 - 0. 00838 - 0. 00409
0. 0 0 6 9 0 0 . 0 0 9 7 3 0. OHIO 0 . 0 1 1 5 3 0 . 0 1 0 5 6
0 . 0 0 178 0 . 0 0 4 4 1 0 . 0 0 6 3 7 0 . 0 0 8 7 1 0 . 0 0 9 7 2
+ 0.00026 - 0 . 0 0 1 0 3 - 0 . 0 0 2 4 3 - 0 . 0 0 4 8 1 - 0 . 0 0 6 4 6
5. 0 6.0 7-0 8.0 9.0
10. 0
+ 0 . 2 3 6 3 3 + 0 . 2 2 584 + 0 . 2 1 7 3 0 + 0 . 2 1 0 1 6 + 0 . 2 0 4 0 8 + 0 . 19875
+ 0 . 19823 + 0. 19206 + 0 . 18686 + 0 . 18236 + 0. 17840 + 0. 17488
+ 0 . 12817 + 0 . 12849 + 0 . 12831 + 0 . 12802 + 0 . 12750 + 0 . 12691
+ 0.06523 + 0.06935 + 0.07244 + 0.07485 + 0.07676 + 0.078 30
+ 0 . 0 2 2 6 1 + 0 . 0 2 7 3 6 + 0 . 0 3 1 2 7 + 0 . 0 3 4 5 4 + 0 . 0 3 7 3 2 + 0 . 0 3 9 7 1
- 0 . 0 0 0 2 5 + 0 . 0 0 3 2 4 + 0. 0 0 6 3 6 + 0. 00913 + 0 . 0 1 1 6 1 + 0 . 0 1 3 8 5
0. 0 0 9 0 6 0. 0073 7 0. 0 0 5 6 5 0 . 0 0 3 9 5 0 . 0 0 2 3 2 0. 0 0 0 7 6
0.00996 0.00976 0.00929 0.00868 0. 00796 0.00720
- 0 . 0 0 7 5 3 - 0. 008 19 - 0 . 0 0 8 5 7 - 0 . 0 0 8 70 - 0 . 0 0 8 6 9 - 0 . 0 0 8 58
-
D I A G R A M N9. I APPENDIX B
EFFECTIVE WIDTH OF THE ORTHOTROPIC DECK PLATE. d o AND Co = EFFECTIVE WIDTH OF THE DECK PLATE.
OL AND IDEAL SPANS OF T - R I B S . BOX-RIBS OR FLOOR BEAMS.
h g o C L * OR e0 1.100 1.050 1.000 0.9 50 0.900 0.8 50 0.800 0.7 50 0.700 0.6 50 0.600 0.5 50 0.500 0.450 0.4OO 0.350 0.300 0.250 0.200 0.1 50 0.100 0.050 0.000
960'
1
-
680'1 1.08
5
1.05
9
- -
1.04
3
-
\ .
0.98
9
0.95
6
0.93
0
- -
0.89
2
0.8
70
_ 5
0.82
6 0.
798
--
0.76
2
-
0.73
2
-
0.69
8
^
0.68
3
-
0.64
3
0.61
8
0.59
1 0.
560
-
0.54
0
0.52
0
\
0.50
5
0.48
5
0.46
8 0.
448
0.43
0 0.
420
0.40
5
a
a
e D
sea* jcL* 0.0 0.1 0.2 0.3 0.4 0.5 0.6 Q7 0.8 0.9 1.0 I.I 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0 OR e, b
.
I
-
. . . . . . . . .
.
T o
-L q
IT o 10
d
- j r > 0.95
0.90
0.85
0.80
0.75
0.70
0.65
0.60
0.55
0.50
0.45
0.40
0.35
0.30
0.25
0.20
0.15
0.10
0.05
0.00 0
D I A G R A M No. 2 LOADING DISTRIBUTION
CO 0 1 0> o
0.60
0
0
0,99
3 ^
0.59
9
0
0,98
4 0.
598
-
2
I*: N 0!
d m t n i n
6
-
-
0
0.95
9 0.
59 2
-
-
4
OJ 1 01
a
0.58
9
-
-
1
0
t o OJ o i
d
0.58
4
-
-
-
6
0.90
2 0.
57 9
-
-
-
0
0.87
9 0.
57 3
-
-
8
0.85
4 0.
567
-
1
0 62
8 0.
56
1
-
0
0.80
1 0.
553
--
'
0.77
3 0.
546
-
(
2
0.74
4 10
.534
-
(1=1
1
0.7
14 _
0.52
7
J
4
0.67
8
m 6
1.
0.65
4
1 O
6
I -
-
6
m OJ ID
6
0.49
4
-
-
'
0.59
6 0.
482
-
-
N
-
8
0.56
7 0.
471
-
2.
0.53
9 0,
459
0
0.5
12
0.44
7
-
2
0.48
6 0.
436
_
m
2
r o IS 1
6 OJ r j T
6
2
0 d
0.41
1
4
0.4
17
en 01 r o
-
-
2
CO 0 1 t o
d
CO t o
o
-
-
6
0.37
9
lO
6
-
2
0.36
1
t o t o t o
d
-
8
m t o
O
o IO
6
-
3
t o
O
t o t o O
-
-
0
m t o
6
0.32
6
-
-
3.
0.30
2
CO
t o
o
-
2
o> (M O
CO O t o
6
3
O CO (\> O CO 0 1 OJ
o
"
-
4
0.27
1
CO CO
2
-
5
-
3.
t o CO OJ
O
0.27
7
-
-
6
0.25
5
0 1 CD OJ O
-
3.
CO OJ
O
0,26
0 8
OJ
6 t o i n OJ
6
1 B
inn >
APPENDIX B
P ^
i i i 3 2 1 0 1 2 3 1 * 1 < - - 1 1 I 1
L U R. R R. V
1 1 _a__
1 i i i
.a 1 a l a j
u B . P 1 1 s~ r
1 i mw
1 1 1 1 1 1 1 1 3 2 1 0 0 1 2 3 | . | . | , * . | a . | , a , | . a , | . a , |
R. R. R. R.
1 1 1 , ., I , . | .
a | a I a ' " '
1 1 a 1 a 1
B 4.0 a
-
to CO
ct a
D I A G R A M No. 3 IDEAL SPACING OF FLEXIBLE RIBS.
2.00
0 1=1
1.
700
2 . 0 0
1.90
1.80
1 7 0
1.60
1 5 0
1 4 0
1 3 0
1 2 0
1 10
1,00
0 . 9 0
0 .80
0 .70
0 6 0
0 5 0
0 30
0 2 0
O.OO
1.99
8
o o
1.99
3
8691
1.98
4 1.
696
01
o ei 10
01 m 01
1.68
4 1.
941
1.92
0 1
1.67
8 1.
668
1.89
7 1.
658
1.87
1 1.
646
CM 0 * CO CO CO N
1.63
4 O to CM O to to
1.74
4 1.
592
(
1.70
7 1.
568
1=1
1.66
7 1.
554
f"-
)
IO
1.52
8 1.
582
1.50
8 1.
539
1.48
8
I
1.49
4 1.
464
1.44
8 1.
442
o
1.4
18
in
1.39
4 1.
309
1.37
0
to 10 cy
1.34
4
-'
1.22
3 1.
322
CO
1.29
8 1.
135
! 1.
274
O o
1.24
0
O
1.22
6
(O o
1.20
0
in
o
ID
0.9
59
1.15
2 0.
928
1.13
2 0
.90
2 0.
87 5
-
0.00 I I I I I 1 I I I I 11 1 I 11 I I I I I I I . 0.0 0.2 0.4 0.6 0.B 1.0 1.4 1.8 2.0 2.2 2.4 2.6 2.8 3.0 3.2 3.4 3.6 3.8 4.0
D I A G R A M No. 4 A P P E N D I X B
ORDINATES FOR INFLUENCE LINES FOR CONTINUOUS BEAM OVER MULTIPLE RIGID. SUPPORTS.
[-0
Cn
n =i Tt = O -n. = i
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