Use the moment-distribution method to determine the moment at each joint of the frame. The supports at
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500 lb/ft By | ]2.5 ft 2.5 Г. - 6 ft- - 6 ft- -18 ft 1 ft 1 ft- -1 ft 20 ft A. TABLE 13-1 Straight Haunches-Constant Width Note: All carry-over factors are negative and all stiffness factors are positive. Concentrated Load FEM-Coef. x PL Haunch Load at ь Left Right Unif. Load FEM Coef x wal FEM Right Haunch Stiffness Factors Coef x waL? 0.1 Carry-over Factors FEM Coef. X wl? 0.3 0.5 0.7 0.9 CAB СвА КАв kBA MAB MBa МАв MBA Mав МвA MAB MBA Mas MBA Maa MBA Мав MBA MAB aA- 0.3 ag- variable TA- 1.0 ra- variable 0.4 0.0935 0.0034 0.2185 0.0384 0.1955 0.1147 0.0889 0.1601 0.0096 | 0.0870 0.0133 0.0008 0.0006 0.0058 0.0038 0.2158 0.0422 0.1883 0.1250 0.0798 0.1729 0.0075 0.0898 0.0133 0.543 0.766 9.19 6.52 0.1194 0.0791 0.6 | 0.576 0.758 9.53 7.24 0.1152 0.0851 0.0934 0.0009 | 0.0005 0.0060 10 0.622 0.0042 0.2118 0.0480 0.1771 0.0011 | 0.0004 0.0062 0.1411 0.0668 0.1919 0.0047 0.0530 0.1678 0.1550 0.0559 0.2078 0.0028 0.0961 0.2 0.748 10.06 8.37 0.1089 0.0942 0.0931 0.0935 0.0132 15 0.660 0.0927 0.0130 0.0012 0.0002 0.0064 0.0565 0.1614 0.1645 0.0487 0.21850.0019 0.0974 0.0129 0.0013 0.0001 0.0065 0.740 10.52 9.38 0.1037 0.1018 0.0047 0.2085 2.0 0.684 0.734 10.83 10.09 0.1002 0.1069 0.0924 0.0050| 0.2062 0.0419 0.1909 0.1225 0.0856 0.1649 0.0100 0.0861 0.0042| 0.2126 0.0477 0.1808 0.1379 0.0747 0.1807 0.0080 O.0888 0.0934 0.0133 0.0009 0.0022 0.0118 0.0010 | 0.0018 0.0124 0.4 0.579 0.741 9.47 7.40 0.1175 0.0822 0.0037 0.2164 0.6 0.629 0.726 9.98 8.64 0.1120 0.0902 0.0931 0.0132 1.0 0.705 0.0924 0.0052 0.2063 0.0577 0.1640 0.1640 0.0577 0.20630.0052 0.0924 0.0131 0.0675 0.1483 0.1892 0.0428 0.2294|0.0033 0.0953 0.0129 | 0.0015 | 0.0008 0.3 0.705 10.85 10.85 0.1034 0.1034 0.0013 0.0013 0.0131 15 0.771 0.689 11.70 13.10 0.0956 0.1157 0.0917 0.0062 0.2002 0.0137 2.0 0.817 0.678 12.33 14.85 0.0901 0.1246 0.0913 0.0069 0.1957 0.0750 0.1368 0.2080 0.0326 0.2455 0.0022 0.0968 0.0128 0.0017 | 0.0006 0.0141 aA - 0.2 ag- variable ГА 1.5 ra- variable 0.4 0.569 0.0966 0.0019 | 0.2186 | 0.0377 0.1847 |0.1183 0.0821 0.1626 0.0088 0.0873 0.0064 | 0.0001 | 0.0006 0.0058 0.0021| 0.2163 0.0413 0.1778 0.1288 0.0736 0.1752 0.0068 | 0.0901 0.0064 0.0001 | 0.0005 0.0060 0.0002 0.0004 0.0062 0.714 7.97 6.35 0.1166 0.0799 0.6 0.603 0.707 8.26 7.04 0.1127 0.0858 0.0965 1.0 0.652 0.0468 0.1675 0.1449 0.0616 0.19400.0043 0.0937 0.2097| 0.0515 0.1587 0.1587 0.0515 0.2097 0.0025 0.0962 0.0064 0.0547 0.1528 0.1681 0.0449 0.22020.0017 0.0975 0.0064 0.2 0.698 8.70 8.12 0.1069 0.0947 0.0963 0.0023 0.2127 0.0064 15 0.691 0.691 9.08 9.08 0.1021 0.1021 0.0962 0.0025 0.0002 | 0.0002 0.0064 2.0 0.716 0.686 9.34 9.75 0.0990 0.1071 0.0960 0.0028 0.2077 0.0002| 0.0001 0.0065 0.4 0.607 0.692 8.21 7.21 0.1148 0.OR29 0.0965 0.0021 0.2168 0.0409 0.1801 0.1263 0.0789 0.1674 0.0091 0.0866 0.0064 0.0002 | 0.0020 0.0118 0.6 0.659 0.0907 0.0464 0.1706 0.1418 0.0688 0.18310.0072 0.0892 0.0064 0.0002 | 0.0017 0.0123 0.0002 0.0012 0.0130 0.678 8.65 8.40 0.1098 0.0964 0.0024 0.2135 1.0| 0.740 0.1037 0.0961 0.0559 0.1550 0.1678 0.0530 0.20850.0047 0.0927 0.0064 0.1928 0.0393 0.2311 0.0029 0.0950| 0.0063 0.3 0.660 9.38 10.52 0.1018 0.0028 0.2078 1.5 0.809 0.645 10.09 12.66 0.0947 0.1156 0.0958 0.0033 0.2024 0.0651 0.1403 0.0003 0.0008 0.0137 0.857 0.636 10.62 14.32 0.0897 0.1242 0.0955 0.0038 0.1985 0.0720 0.1296 0.2119 0.0299 0.2469 0.0020 0.0968 0.0063 0.0003 0.0005 0.0141
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