Page 323 - Advanced Design Examples of Seismic Retrofit of Structures
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Linear interpolation between the values on lines a and b for both flange slenderness (first term) and web slenderness (second term) shall be performed,
                                   Linear interpolation between the values on lines a and b for both flange slenderness (first term) and web slenderness (second term) shall be performed,
                   Radians
                           11θ y
                                             11θ y
                      CP
                               4θ y
                                                 4θ y
                                                            – d
                   Angle,
                   Rotation
                      LS
                           9θ y
                               3θ y
                                                 3θ y
                                             9θ y
                                                            – e
                   Plastic
                                                            0.25θ y
                                                 0.25θ y
                               0.25θ y
                                             1θ y
                      IO
                           1θ y
                   Ratio
                   Strength
         for  [3] Components  Steel Procedures-Structural Nonlinear  Parameters Modeling  312 Criteria Acceptance  Advanced Design Examples of Seismic Retrofit of Structures  1.2θ y 1.2θ y 0.25θ y Linear interpolation between the values on lines a and b for both flange slenderness (first term) and web slenderness (second term) shall be perfor
                   Residual
         Criteria     c    0.6  0.2          0.6  0.2       0.2  0.2      for  designed  190.
         Acceptance  Angle,  b  11θ y  6θ y  and the lower resulting value shall be used.  11θ y  6θ y  and the lower resulting value shall be used.  – d  1.5θ y  and the lowest resulting value shall be used.  be  to  with  65  controlled.  bending.  bending.  bending.
         and     Rotation                                                 permitted  be  replace  and  force  of  plane  of  plane  of  plane
         Parameters  Plastic  Radians  a  9θ y  4θ y  9θ y  4θ y  – c  1θ y  shall  frames  110,  with  52  considered  be  the  in  P/P CL )θ y  the  in  P/P CL )θ y  the  in  P/P CL )θ y
         Modeling     Action  or  418  h   p  ffiffiffiffiffi  F ye  640  ffiffiffiffiffi  F ye  300  h   p  ffiffiffiffiffi  F ye  460  ffiffiffiffiffi  F ye  260  h   p  ffiffiffiffiffi  F ye  400  ffiffiffiffiffi  F ye  braced  or  moment  replace  b/t,  shall P/P CL >0.5  rotation¼11(1 5/3  rotation¼17(1 5/3  rotation¼14(1 5/3
         5.12              ffiffiffiffiffi and  t w  F ye  h   p  ffiffiffiffiffi or  t w  F ye  Columns—flexure a,b  and  ffiffiffiffiffi  t w  F ye  h   p  or  ffiffiffiffiffi  t w  F ye  For 0.2 P/P CL  0.5  ffiffiffiffiffi and  t w  F ye  h   p  ffiffiffiffiffi or  t w  F ye  in  with  b t /2t f  with
         TABLE        Component  Beams—flexure  52  b f a: 2t f   p  65  b f  b: 2t f   p  c: Other  For P/P CL <0.2  52  b f a: 2t f   p  65  b f b: 2t f   p  c: Other  b f  52  a: 2t f   p  b f  65  b: 2t f   p  c: Other  a Columns  replace  b Columns  c Plastic  d Plastic  e Plastic
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