Page 132 - Handbook of Civil Engineering Calculations, Second Edition
P. 132

STRUCTURAL STEEL DESIGN               1.115

                                Expressing the relationships among
                              the tensile stresses, we have   L
                              s A L A /E   s B L B /E   s C L C /E; therefore,
                              s A   s C , and s A   s B L B /L A   0.75s B
                              for this arrangement of rods. Since s B
                              is the maximum stress, the allowable
                              stress first appears in rod B.
                              2. Evaluate the stresses at the
                              instant the load attains its
                              allowable value
                              Calculate the load carried by each rod,
                              and sum these loads to find  P allow .
                              Thus s B   22,000 lb/sq.in. (151,690.0
                              kPa);  s B   0.75(22,000)    16,500  FIGURE 19
                              lb/sq.in. (113,767.5 kPa); P A   P C
                              16,500(1.2)    19,800 lb (88,070.4
                              N); P B   22,000(1.0)   22,000 lb (97,856.0 N); P allow   2(19,800) + 22,000   61,600 lb
                              (273,996.8 N).
                                Next, consider that the load is gradually increased from zero to its ultimate value.
                              When rod B attains its yield-point stress, its tendency to deform plastically is inhibited by
                              rods A and C because the rigidity of the bar constrains the three rods to elongate uniform-
                              ly. The structure therefore remains stable as the load is increased beyond the elastic range
                              until rods A and C also attain their yield-point stress.
                              3. Find the ultimate load
                              To find the ultimate load P u , equate the stress in each rod to f y , calculate the load carried by
                              each rod, and sum these loads to find the ultimate load P u . Thus, P A   P C   36,000(1.2)
                              43,200 lb (192,153.6 N); P B   36,000(1.0)   36,000 lb (160,128.0 N); P u   2(43,200) +
                              36,000   122,400 lb (544,435.2 N).
                              4. Apply the load factor to establish the allowable load
                              Thus, P allow   P u /LF   122,400/1.85   66,200 lb (294,457.6 N).


                              DETERMINATION OF SECTION
                              SHAPE FACTORS

                              Without applying the equations and numerical values of the plastic modulus given in the
                              AISC Manual, determine the shape factor associated with a rectangle, a circle, and a W16
                              40. Explain why the circle has the highest and the W section the lowest factor of the three.


                              Calculation Procedure:
                              1. Calculate M y for each section
                                                                                    2
                              Use the equation M y   Sf y for each section. Thus, for a rectangle, M y   bd f y /6. For a cir-
                                                                                      3
                              cle, using the properties of a circle as given in the Manual, we find M y    d f y /32. For a
                                                           2
                                                                                3
                                                                      3
                              W16   40, A   11.77 sq.in. (75.940 cm ), S   64.4 in (1055.52 cm ), and M y   64.4f y .
                              2. Compute the resultant forces associated with plastification
                              In Fig. 20, the resultant forces are C and T. Once these forces are known, their action lines
                              and M p should be computed.
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