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7
CONTINUOUS INFLUENCE LINES FOR. 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 -0.0008 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 -0.00005 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 -0.00816 - 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 -0.00328 + 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

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  • 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

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    APPENDIX B

    P ^

    i i i 3 2 1 0 1 2 3 1 * 1 < - - 1 1 I 1

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    1 1 _a__

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    D I A G R A M No. 3 IDEAL SPACING OF FLEXIBLE RIBS.

    2.00

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    1.80

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    1.60

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    1.89

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    1.87

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    CM 0 * CO CO CO N

    1.63

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    1.74

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    1.52

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    539

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  • 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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