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                 504   Mechanical Engineering Design
                  Figure 9–27                             Shear stress   (psi)

                  Plot for Ex. 9–7.                         4000
                                                                                     Combined
                                                            3000
                                                            2000                      Thermal
                                                            1000                    Load induced

                                                                                     x (in)
                                              −0.4   −0.2              0.2     0.4
                                                           −1000
                                                           −2000



                                          τ avg = P/(2bl) = 1000 psi. Equation (1) produced a maximum of 1922 psi, almost
                                          double the average.





                                              Although design considerations for single-lap joints are beyond the scope of this
                                          chapter, one should note that the load eccentricity is an important aspect in the stress
                                          state of single-lap joints. Adherend bending can result in shear stresses that may be as
                                          much as double those given for the double-lap configuration (for a given total bond area).
                                          In addition, peel stresses can be quite large and often account for joint failure. Finally,
                                          plastic bending of the adherends can lead to high strains, which less ductile adhesives
                                          cannot withstand, leading to bond failure as well. Bending stresses in the adherends at
                                          the end of the overlap can be four times greater than the average stress within the
                                          adherend; thus, they must be considered in the design. Figure 9–28 shows the shear and
                                          peel stresses present in a typical single-lap joint that corresponds to the ASTM D1002
                                          test specimen. Note that the shear stresses are significantly larger than predicted by the
                                          Volkersen analysis, a result of the increased adhesive strains associated with adherend
                                          bending.

                                          Joint Design
                                          Some basic guidelines that should be used in adhesive joint design include:
                                          • Design to place bondline in shear, not peel. Beware of peel stresses focused at bond
                                            terminations. When necessary, reduce peel stresses through tapering the adherend
                                            ends, increasing bond area where peel stresses occur, or utilizing rivets at bond termi-
                                            nations where peel stresses can initiate failures.
                                          • Where possible, use adhesives with adequate ductility. The ability of an adhesive to
                                            yield reduces the stress concentrations associated with the ends of joints and increases
                                            the toughness to resist debond propagation.
                                          • Recognize environmental limitations of adhesives and surface preparation methods.
                                            Exposure to water, solvents, and other diluents can significantly degrade adhesive
                                            performance in some situations, through displacing the adhesive from the surface or
                                            degrading the polymer. Certain adhesives may be susceptible to environmental stress
                                            cracking in the presence of certain solvents. Exposure to ultraviolet light can also
                                            degrade adhesives.
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