Page 190 - Civil Engineering Formulas
P. 190

126                     CHAPTER FIVE

                 t   diameter of column or overall depth of column, in (mm)
                 d   distance from extreme compression fiber to centroid of tension rein-
                    forcement, in (mm)
                                             2
                 f   yield point of reinforcement, lb/in (MPa)
                 v
             Design of columns controlled by compression  is based on  the following
           equation, except that the allowable load N may not exceed the allowable load P,
           given earlier, permitted when the column supports axial load only:
                                f a  f bx  f by
                                              1.0               (5.21)
                               F a  F b   F b
                                                         2
           where   f   axial load divided by gross concrete area, lb/in (MPa)
                    a
                f , f   bending moment about x and y axes, divided by section modulus
                   by
                 bx
                                                              2
                       of corresponding transformed uncracked section, lb/in (MPa)
                   F   allowable bending stress permitted for bending alone, lb/in 2
                    b
                       (MPa)
                   F   0.34(1   p m) f  c
                    a
                               g
             The allowable bending load on columns controlled by tension varies linearly
           with the axial load from M when the section is in pure bending to M when the
                                                             b
                              0
           axial load is N .
                     b
             For spiral columns,
                                                                (5.22)
                                 M 0   0.12A st f y D s
             For tied columns,
                               M 0   0.40A s f y (d   d )       (5.23)
                                                    2
                                                2
           where A   total area of longitudinal reinforcement, in (mm )
                 st
                f   yield strength of reinforcement, lb/in (MPa)
                                              2
                 v
                D   diameter of circle through centers of longitudinal reinforcement, in
                 s
                    (mm)
                                           2
                                                2
                A   area of tension reinforcement, in (mm )
                 s
                 d   distance from extreme compression fiber to centroid of tension rein-
                    forcement, in (mm)
           N and M are the axial load and moment at the balanced condition (i.e., when
                  b
            b
           the eccentricity e equals e as determined). At this condition, N and M should
                                                         b
                              b
                                                               b
           be determined from
                                    M b   N b e b               (5.24)
           When bending is about two axes,
                                  M x   M y
                                             1                  (5.25)
                                  M 0x  M 0y
   185   186   187   188   189   190   191   192   193   194   195