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                              Table 7.2.
                                      Mechanical properties of common metals and alloys (typical values at room temperature)
                                               Tensile  CHEMICAL ENGINEERING
                                                          0.1 per cent
                                                                       Modulus of
                                               strength   proof stress  elasticity   Hardness   Specific
                                                   2
                                                                2
                                                                             2
                                               (N/mm )     (N/mm )      (kN/mm )     Brinell    gravity
                           Mild steel           430          220          210        100 200      7.9
                           Low alloy steel     420 660     230 460        210        130 200      7.9
                           Cast iron           140 170                    140        150 250      7.2
                           Stainless steel
                             (18Cr, 8Ni)       >540          200          210         160         8.0
                           Nickel
                             (>99 per cent Ni)  500          130          210        80 150       8.9
                           Monel                650          170          170        120 250      8.8
                           Copper
                             (deoxidised)       200          60           110        30 100       8.9
                           Brass
                             (Admiralty)       400 600       130          115        100 200      8.6
                           Aluminium
                             (>99 per cent)    80 150                      70          30         2.7
                           Dural                400          150           70         100         2.7
                           Lead                  30                        15           5        11.3
                           Titanium             500          350          110         150         4.5
                           7.3.3. Toughness
                           Toughness is associated with tensile strength, and is a measure of the material’s resistance
                           to crack propagation. The crystal structure of ductile materials, such as steel, aluminium
                           and copper, is such that they stop the propagation of a crack by local yielding at the crack
                           tip. In other materials, such as the cast irons and glass, the structure is such that local
                           yielding does not occur and the materials are brittle. Brittle materials are weak in tension
                           but strong in compression. Under compression any incipient cracks present are closed up.
                           Various techniques have been developed to allow the use of brittle materials in situations
                           where tensile stress would normally occur. For example, the use of prestressed concrete,
                           and glass-fibre-reinforced plastics in pressure vessels construction.
                             A detailed discussion of the factors that determine the fracture toughness of materials
                           can be found in the books by Institute of Metallurgists (1960) and Boyd (1970). Gordon
                           (1976) gives an elementary, but very readable, account of the strength of materials in
                           terms of their macroscopic and microscopic structure.

                           7.3.4. Hardness
                           The surface hardness, as measured in a standard test, is an indication of a material’s ability
                           to resist wear. This will be an important property if the equipment is being designed to
                           handle abrasive solids, or liquids containing suspended solids which are likely to cause
                           erosion.

                           7.3.5. Fatigue
                           Fatigue failure is likely to occur in equipment subject to cyclic loading; for example,
                           rotating equipment, such as pumps and compressors, and equipment subjected to pressure
                           cycling. A comprehensive treatment of this subject is given by Harris (1976).
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