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                 254    Mechanical Engineering Design


                                           1                    1

                                          R                     R 2
                                           2




                                                    R 1   1              R 1    1
                                                    (a)                  (b)
                                           Figure 5–33

                                           Curve shapes of the R 1 R 2 plot. In each case the shaded area
                                           is equal to 1 − R and is obtained by numerical integration.
                                           (a) Typical curve for asymptotic distributions; (b) curve shape
                                           obtained from lower truncated distributions such as the Weibull.

                                          where
                                                                             ∞

                                                                   R 1 (x) =   f 1 (S) dS                  (5–47)
                                                                            x

                                                                             ∞
                                                                   R 2 (x) =   f 2 (σ) dσ                  (5–48)
                                                                            x
                                          For the usual distributions encountered, plots of  R 1 versus  R 2 appear as shown in
                                          Fig. 5–33. Both of the cases shown are amenable to numerical integration and com-
                                          puter solution. When the reliability is high, the bulk of the integration area is under the
                                          right-hand spike of Fig. 5–33a.
                                5–14      Important Design Equations

                                          The following equations and their locations are provided as a summary. Note for plane
                                          stress: The principal stresses in the following equations that are labeled σ A and σ B rep-
                                          resent the principal stresses determined from the two-dimensional Eq. (3–13).
                                          Maximum Shear Theory

                                                                          σ 1 − σ 3  S y
                                          p. 220                    τ max =      =                          (5–3)
                                                                            2      2n
                                          Distortion-Energy Theory
                                            Von Mises stress, p. 223

                                                                      2          2          2    1/2
                                                               (σ 1 − σ 2 ) + (σ 2 − σ 3 ) + (σ 3 − σ 1 )
                                                                                                           (5–12)
                                                         σ =
                                                                             2
                                                                                                           1/2
                                                       1          2         2          2     2    2    2

                                          p. 223 σ = √    (σ x − σ y ) + (σ y − σ z ) + (σ z − σ x ) + 6(τ xy  + τ + τ )
                                                                                                  yz
                                                                                                       zx
                                                       2
                                                                                                           (5–14)
                                            Plane stress, p. 223
                                                                                 2 1/2
                                                                      2

                                                               σ = (σ − σ A σ B + σ )                      (5–13)
                                                                      A          B
                                                                      2
                                                                                      2
                                                                                 2
                                          p. 223               σ = (σ − σ x σ y + σ + 3τ ) 1/2             (5–15)

                                                                     x          y     xy
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