Page 174 - Shigley's Mechanical Engineering Design
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                                                                                              Deflection and Stiffness  149
                                               as shown by the graph. Any mechanical element having such a characteristic is called a
                                               nonlinear softening spring.
                                                  If we designate the general relationship between force and deflection by the equation

                                                                             F = F(y)                             (a)
                                               then spring rate is defined as
                                                                                   F    dF
                                                                       k(y) = lim     =                         (4–1)
                                                                               y→0  y    dy
                                               where y must be measured in the direction of F and at the point of application of F. Most
                                               of the force-deflection problems encountered in this book are linear, as in Fig. 4–1a. For
                                               these, k is a constant, also called the spring constant; consequently Eq. (4–1) is written
                                                                                   F
                                                                               k =                              (4–2)
                                                                                   y
                                               We might note that Eqs. (4–1) and (4–2) are quite general and apply equally well for
                                               torques and moments, provided angular measurements are used for y. For linear dis-
                                               placements, the units of k are often pounds per inch or newtons per meter, and for
                                               angular displacements, pound-inches per radian or newton-meters per radian.

                                       4–2     Tension, Compression, and Torsion

                                               The total extension or contraction of a uniform bar in pure tension or compression,
                                               respectively, is given by
                                                                                  Fl
                                                                              δ =                               (4–3)
                                                                                  AE
                                               This equation does not apply to a long bar loaded in compression if there is a possibil-
                                               ity of buckling (see Secs. 4–11 to 4–15). Using Eqs. (4–2) and (4–3) with δ = y, we see
                                               that the spring constant of an axially loaded bar is
                                                                                  AE
                                                                              k =                               (4–4)
                                                                                   l
                                                  The angular deflection of a uniform solid or hollow round bar subjected to a twist-
                                               ing moment T was given in Eq. (3–35), and is
                                                                                  Tl
                                                                              θ =                               (4–5)
                                                                                  GJ
                                                                                                              4
                                               where θ is in radians. If we multiply Eq. (4–5) by 180/π and substitute J = πd /32 for
                                               a solid round bar, we obtain
                                                                                583.6Tl
                                                                            θ =                                 (4–6)
                                                                                  Gd 4
                                               where θ is in degrees.
                                                  Equation (4–5) can be rearranged to give the torsional spring rate as
                                                                               T    GJ
                                                                           k =    =                             (4–7)
                                                                                θ    l
                                               Equations (4–5), (4–6), and (4–7) apply only to circular cross sections. Torsional load-
                                               ing for bars with noncircular cross sections is discussed in Sec. 3–12 (p. 101). For the
                                               angular twist of rectangular cross sections, closed thin-walled tubes, and open thin-
                                               walled sections, refer to Eqs. (3–41), (3–46), and (3–47), respectively.
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