Page 467 - Corrosion Engineering Principles and Practice
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434    C h a p t e r   1 1                                                                   M a t e r i a l s   S e l e c t i o n ,   Te s t i n g ,   a n d   D e s i g n   C o n s i d e r a t i o n s    435


                      aircraft in which rivets have been known to fracture due to the high
                      tensile stresses resulting from pillowing [4].
                      11.2.2  Multiple Material/Environment Combinations
                      There  are  a  vast  number  of  material/operational  environment
                      combinations,  and  each  can  form  the  basis  for  potential  corrosion
                      problems to occur. Of the 103 plus elements in a Periodic Table in App.
                      B, approximately 80 are metals, each possessing different mechanical,
                      chemical, and physical properties. Although all these metals can corrode,
                      they do it in many different manners. Furthermore, most of these metals
                      have been alloyed to make tens of thousands of different alloys.
                         From  a  purely  technical  standpoint,  an  obvious  answer  to
                      corrosion problems would be to use more resistant materials. In many
                      cases, this approach is an economical alternative to other corrosion
                      control methods. Table 11.1 lists the questions that should be answered
                      in  order  to  estimate  the  corrosion  behavior  of  materials  either  in
                      service or considered for such usage [5].
                         A  common  form  of  representing  the  corrosion  resistance  of
                      materials is what is known as isocorrosion diagrams. The use of the
                      prefix “iso” refers to lines (or regions) of constant corrosion behavior
                      across  variations  in  concentration  and  temperature.  The  diagram
                      shown in Fig. 11.2 illustrates how some stainless steels compare to


                  •  Corrosive Agent Variables
                  Main constituents (identity and amount)
                  Impurities (identity and amount)
                  Temperature
                  pH
                  Degree of aeration
                  Velocity or agitation
                  Pressure
                  Estimated range of each variable
                  •  Type of Application
                  What is the function of part or equipment?
                  What effect will uniform corrosion have on serviceability?
                  Are size change, appearance or corrosion product a problem?
                  What effect will localized corrosion have on usefulness?
                  Will there be stresses present?
                  Is SCC a possibility?
                  Is design compatible with the corrosion characteristics of the material?
                  What is the desired service life?

                 TABLE 11.1  Information Required for Estimating the Corrosion Performance of
                 a Material
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