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WORKSHOP CALCULATION & SCIENCE  - CITS



           EXERCISE 16 : Stress and Strain


           Heat & Temperature
           Concepts
           -   Stress is the force applied per unit area of a material. It represents the internal resistance of a material to
              deformation.
           -   Strain is the measure of deformation or change in shape experienced by a material in response to stress. It’s
              usually expressed as the ratio of the change in dimension to the original dimension.
           -   When a material is subjected to stress, it undergoes deformation, and the relationship between stress and
              strain provides valuable information about the material’s mechanical properties.
           Material Properties
           Strength
           Strength is defined us the ability of a material that can withstand to mechanical load or that can resist the maximum
           stress.
           Hardness
           Hardness is the property which is usually defined as the ability of a material to resist scratching, abrasion, cutting
           ( or machining and indentation (or penetration ).
           Toughness
           Toughness is defined as the ability of the material to absorb energy up fracture during to plastic deformation.
           Plasticity
           If a material does not retain the original shape after removal of load is known as plasticity.
           Elasticity
           The elasticity is the ability of material that can regain its original shape after removal of load
           Elastic material The Elastic materials are those materials that have the ability to resist a distorting or deforming
           influence or force, and then return to their original shape and size when the same force is removed. Linear elasticity
           is widely used in the design and analysis of structures such as beams, plates and sheets. Elastic materials are of
           great importance to society since many of them are used to make clothes, tires, automotive spare parts
           Stress
           The internal opposite force to the external load per unit area is known as stress. The unit of stress depends upon
           the force applied and area of original cross-section of material. It is represented by (Sigma)
           Stress =(force applied)/( original Cross Sectional Area)          π 2   π


                                 applied
                           Force
                                                                              d =

                          Force
              Stress =  Original   cros  secti    area                      π 2 4  π 4
                               appliedonal s
                                                                             d =
           Stress =
                   Original   cross   sectional   area                     4     4
                                                                             Load   500    500
                σ = Load   (or)   forced  =  N                        Stress =  Area  =  = 500 22
                                                                           Load
                                                                                  500 16π
                                                                                         16x
               σ =  Load   (or)   Area  =  N  2                    Stress =  Area  = 16π  = 16x  227
                         forced
                                  mm
                     Area       mm  2                                                       7
                                                                              500x7
           Types of Stress                                                  500x7
                                                                             =
                                                                              16x22

                       stress
                    E =
           1   Tensile stress                                              =
                        stre
                      stressin                                               16x22
                  E =
           2   Compressive stress                                    Spring   stiffness =  Applied   load
                      strein
                      shear

                                                                                         load
                                                                                    Defle
           3   Shear stress     stress                              Spring   stiffness =  Applied  ction
                  G =
                    shear   straa stressin r                                       Deflection
                      she
                G =
           4   Torsional Stress                                                               10
                    shear   strain                                         600   newtons
           Tensile stress       stress                                    600 30   mm       10 30
                                                                             newtons


                     volumetric
                                                                                            30
                 K =
           When a material is subjected to two equal and opposite axial pulls, the material tends to increase in length. The
                                                                              mm
                                                                            30


                     volumet
                             stressin c
                   volumetricr
                              strai
               K =
           resistance offered against this increase in length is called tensile stress. The corresponding strain is called tensile

                                                                                     Ultimate
                                                                                             stress

                   volumetric

                             strain
                                                                     Factor
           strain.                                                   Factor   of   of   Safety =  Safe   stress  stress
                                                                                   Ultimate
                                                                           Safety =

               Poisson'    s ratio =  Lateral   strain                               Safe   stress
              Poisson'    s ratio = Lateral   stra                        Safe   stress =  Ultimate    stress
                                  strainin r
                             Linea
                           Linear   strain                              Safe   stress =  Ultimate   stress  stress
                                                                                      Safe
                      1+ μ =  E                            159                      Safe   stress
                         E2G                                                      2.5
                                                                                =
                  1+ μ =  2G                                                    2.54
                       μ =  E  − 1                                            =  4
                     μ =  E2G 1                                         Safe   stress =  Ultimate    stress
                          −
                                                                                  Factor
                      2G                                              Safe   stress =  Ultimate    safety of   stress
                                                                                  π
                                                                             2.5 Factor   of 2   safety
                                                                                 ×
                                                                            =
                      E           E                                   2.54  π 4  (4.2)
                                                                                       2
                                    1
                      
                 
                   −  21   E  2G  −1     = 3K  −  + 2            =  4  ×  4 (4.2)
                                     E G
                                  
                              
                                           
                              
                 −  21     −1     = 3K  −  + 2 
                                  1
                
                    2G          G                                      2.5   22
                                                                                            4.2
                                                                                        4.2×
                                                                            =
                                                                                      ×
                        E      3G - E                                2.54 ×  × 22 47× ×  4.2× 4.2
                                                                          =
                  
                   3K   −3 E G       = 3K    -G               4   7× 4 Load  30× 1000
                                 3G
                                      E
                     
                  
                             
                 3K   −3     = 3K                             Working   stress =  =
                 
                                                                                    Area
                                                                                             1000
                      G       G                               Working   stress =  Load  =  30× 600
                         9KG                                                    Area     600
                                                                                     Ultimate
                                                                                             stress

                       =
                        
                      E  9KG + 3KG                                Factor   of   safety =  Workin   stress g
                                                                                            stress
                                                                                    Ultimate
                        
                   E  =                                           Factor   of   safety =
                        G + 3K                                                    Working   stress
                                                                                  450   M.Pa
                                                                                =
                                                                                450 M.Pa 50 M.Pa

                                                                              =
                                                                                 50   M.Pa
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