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LOAD COMNINATION 1: DEAD LOAD + LIVE LOA[i <br />qr <br />UN) <br />0.00 <br />21.83 <br />43.67 <br />65,50 <br />87.3.; <br />109.17 <br />1:1.00 <br />AXIAL <br />FORCE <br />(LB) <br />-5802. <br />-SB02. <br />-5802. <br />-5802. <br />-5802. <br />-5802. <br />-580^c. <br />SHEAF <br />FOFCE <br />(LB) <br />568. <br />SbB. <br />568. <br />56B. <br />g68. <br />`68. <br />56B. <br />FENDING <br />(LB*IN) <br />-7�q58. <br />-62049. <br />-496:�9. <br />-37229. <br />-24819. <br />-12410. <br />TRANSVEFSE <br />DISPL. <br />(IN) <br />LOAC� COMRINATION -2 : DEAD LOAU + UIND LOAA LEFT <br />AT <br />(IN) <br />0.00 <br />21.83 <br />4^a.67 <br />65.50 <br />87.33 <br />109.17 <br />191.00 <br />AXIAL <br />FORCE <br />(LB1 <br />-296?. <br />-^c96:3. <br />-296c. <br />-2963. <br />-�963. <br />-296'.'•. <br />-2963. <br />SHEAR <br />FOFCE <br />(LH) <br />:.'.9. <br />_g,, <br />-404. <br />-775. <br />-1146. <br />-I517. <br />-18B8. <br />AENDING <br />(LB+�IN) <br />30151`, <br />104B5`. <br />100092. <br />8722`. <br />66254. <br />37180. <br />1. <br />-.07 <br />-.01 <br />.02 <br />.03 <br />.03 <br />.02 <br />.00 <br />TRANSVEFSE <br />DISFL, <br />(IN) <br />-1.37 <br />-i.�;� <br />-1.00 <br />-.86 <br />-,g9 <br />-.30 <br />-.00 <br />LOAU COMPINATION -:+ : DEAG LDAP + WIND �OAD RIGHT <br />AT <br />(IN) <br />Q.00 <br />21.83 <br />4:,.67 <br />65,50 <br />B7.:3 <br />109.17 <br />131.00 <br />AXIAL <br />FORCE <br />(LR) <br />`?;1. <br />� 1 <br />I�J�1• <br />-`351. <br />-$S;1. <br />-5351. <br />-`351. <br />-5351. <br />SHEAF <br />FORCE <br />(LR) <br />119. <br />713• <br />1307. <br />1901. <br />2495. <br />3089. <br />�68': . <br />RENIi I NG <br />(:BzIN> <br />-249028. <br />-2^a99^a8. <br />-�178B�. <br />-1B2B6�. <br />-234874. <br />-75922. <br />-2. <br />TRANSVERSE <br />UISFL. <br />(IN) <br />1.56 <br />1.44 <br />1.37 <br />1.12 <br />.80 <br />.41 <br />.00 <br />AXIAL <br />STRESS <br />(LB/IN2) <br />-195q.81 <br />-19`�.82 <br />-195�.8�'. <br />-19gq,82 <br />-1954.82 <br />-1954.82 <br />-1954.82 <br />AXIAL <br />STRESS <br />(LH/IH2> <br />-99B.34 <br />-998.:�4 <br />-998.34 <br />-998.�5 <br />-998.35 <br />-99B.:g <br />-998.35 <br />AXIAL <br />STFESS <br />(LP/IN2) <br />-ieoz.e� <br />-3802.88 <br />-1802.89 <br />-1802.87 <br />-1802.87 <br />-3802.87 <br />-1802.87 <br />LOAD COMNINATION -4 : DEAD LOAb + 1/2 LIVE LOAD + WIND LOAU LEFT <br />AT <br />tIN) <br />0.00 <br />�1.B3 <br />4^a.67 <br />b$,5Q <br />87.?C <br />109.17 <br />131.OG <br />AXIAL <br />FORCE <br />(LF) <br />_"q. . <br />-55g.', <br />_«S? <br />-55`;:. <br />_`�:?. <br />-5`53. <br />-`5.`S. <br />SHEAR <br />FOkCE <br />(LB) <br />592. <br />221. <br />-1g0. <br />-52' . <br />-892. <br />-1.'.63. <br />-1635, <br />EENDING <br />(LFtcIN) <br />68�74. <br />7715g. <br />779;1. <br />i�L04. <br />5`174. <br />31640. <br />1. <br />TRANSVERSE <br />DISF'L. <br />fIN) <br />-1.c:7 <br />'1.25 <br />-1.00 <br />-.84 <br />_.`6 <br />-.29 <br />-.00 <br />AXIAL <br />STRESS <br />(LR/IM2) <br />-1871.04 <br />-1871.0^0 <br />-1871.0^a <br />-1871.04 <br />-1871.04 <br />-IQ71.04 <br />-1871.04 <br />LOAD � INATION c� : PEAP LOA" + 1/2 LIVE LUAll + WINC� LOAD RIGHT <br />BENDING <br />STRESS <br />(LH/IN2) <br />8239.31 <br />6866.11 <br />5�92.88 <br />�119.b6 <br />27�6.�� <br />1?73.22 <br />.O1 <br />AENDING <br />3TRESS <br />tLB/IN2) <br />-112:�^a.31 <br />-11602.9g <br />-11075.87 <br />-965z.04 <br />-7^a31.46 <br />-4114.21 <br />-.16 <br />RENPING <br />STRESS <br />(L6/IN2) <br />�'.7556.66 <br />26550.87 <br />24110.29 <br />20234.94 <br />14924.62 <br />8179.96 <br />.?6 <br />AENOJNG <br />STn'ESS <br />(LB/IN2) <br />_7�55.0^c <br />-8`:�7.70 <br />-8623.66 <br />-7812.88 <br />-61,i5.37 <br />-i`01.16 <br />-.16 <br />SHEAR <br />STRESS <br />fLB/IN2) <br />�97.17 <br />�97.16 <br />�97.17 <br />�97.17 <br />�97.17 <br />�97.17 <br />�97.17 <br />SHEAR <br />STRESS <br />(LB/IN2) <br />296.18 <br />-28.47 <br />-3g3.16 <br />-b77.81 <br />-1002.47 <br />-1327.13 <br />-1651.79 <br />SHEAF <br />STRESS <br />(LA/IN.°) <br />104.40 <br />628.8`? <br />1143.3) <br />1062.%7 <br />2182.2' <br />2701.68 <br />3221.1� <br />SHEAR <br />STRE;S <br />fLF/IN2) <br />Si8.13 <br />19�.48 <br />-131.20 <br />-455,86 <br />-7B0.�2 <br />-1105.x6 <br />-1429.84 <br />