The Theory of Strains a Compendium for the Calculation And Construction of Brid

John H Diedrichs

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R . T) ; / I r t / -/ >? . Xj y SEMI-GIRDERS. LOADED AT EACfl APEX. 45 Q = Xl . L, 8 + P. 4 (rot. /); 1, 8 C, ] = z 2 . 1, 99 + P. 4 (rot. R . E, Fig. C) ; 120000 .
= y, . 4, 4 P-. 1, 2 (rot. R . K) } y 2 = -f 8168 ; 0=z 2 . 3 + P. 8 (rot. R. D); z 2 = 80000; D. ] = z z . 3, 2 + P. 8 (rot. R . C, Fig, D) ; z 3 = 75000 ; = fc, . 4, 2 + P. 12 (rot. R . 6) j * 3 = 85700.
For tfo the intersection of 3 and z 3 is to the left of the sus* pended Weight, and the symbql reversed.
= t/ 3 . 7, 25 -f- P. 2..., 6 (rot. R . F) j y, = 10758, which would be = when the intersection is in the vertical line of the suspended weight, as the lines oe and pc in Fig; A indicate* For the verticals, V, we have from Fig. D, = V 1 . 10, 1 P. 6, 1 (rot. R . M) ; F, = 18118; = V, . 26, 5 P. 18, 5 (rot. R . N) J 7. = _ 20943 E. ] The results combined in Fig. E. * II. SEMZGIRDERS LOADED At EACH APEX.
In Fig. 25 is occasionally explained how to compute the stress in diagonals, as there is no intersection of joining flanges, x and z, and as in the case here considered the diagonals receive at each loaded * For most purpose?

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