Page 281 - Marks Calculation for Machine Design
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P1: Shibu
                                      14:56
                          January 4, 2005
                 Brown˙C06
        Brown.cls
                                     STATIC DESIGN AND COLUMN BUCKLING
                              U.S. Customary                      SI/Metric       263
                    Step 2. Calculate the slenderness ratio (L/k)  Step 2. Calculate the slenderness ratio (L/k)
                             L   72 in                         L    2m
                              =      = 248                      =        = 278
                             k  0.29 in                        k  0.0072 m
                    so the Euler’s Buckling formula applies.  so the Euler’s Buckling formula applies.
                    Step 3. Using Eq. (6.27), calculate the critical  Step 3. Using Eq. (6.27), calculate the critical
                    stress (σ cr ) as                  stress (σ cr ) as
                                                                   2
                                  2
                              C ends π E                      C ends π E
                         σ cr =                          σ cr =
                                   2                               2
                                L                                L
                                k                                k
                                           2
                                       6
                                 2
                                                                         9
                                                                            2
                                                                 2
                              (1)π (30 × 10 lb/in )           (1)π (207 × 10 N/m )
                            =                               =
                                   (248) 2                          (278) 2
                                    6
                                                                     9
                              296 × 10 lb/in 2                2,043 × 10 N/m 2
                            =                               =
                                 61,504                           77,284
                                    2
                                                                         2
                            = 4,813 lb/in = 4.8 kpsi        = 26,435,000 N/m = 26.4MPa
                    Step 4. Using Eq. (6.28), calculate the axial  Step 4. Using Eq. (6.28), calculate the axial
                    stress (σ axial ) as               stress (σ axial ) as
                               P   24,000 lb                   P      108,000 N
                         σ axial =  =                    σ axial =  =
                               A  (1in)(3in)                   A   (0.025 m)(0.075 m)
                                                                         2
                                     2
                             = 8,000 lb/in = 8.0 kpsi        = 57,600,000 N/m = 57.6MPa
                    Step 5. Comparing the critical stress found in  Step 5. Comparing the critical stress found in
                    step 3 with the axial stress found in step 4, it is  step 3 with the axial stress found in step 4, it is
                    clear the design is unsafe as      clear the design is unsafe as
                               σ axial >σ cr                      σ axial >σ cr
                    6.2.2 Parabolic Formula
                    For columns where the slenderness ratio (L/k) is less than a certain value, the Euler formula
                    does not accurately predict column buckling. As mentioned earlier, the Euler formula given
                    in Eq. (6.27) states that the critical stress (σ cr ) is inversely proportional to the square of the
                    slenderness ratio (L/k). This inverse relationship is presented graphically in Fig. 6.21 as the
                    curve from point A to point B.
                      The lower limit of the slenderness ratio for which the Euler formula is appropriate is
                    indicated by point D, denoted (L/k) D , where the critical stress is set equal to the yield
                    stress divided by two (S y /2). The value of the slenderness ratio at this point is given in
                    Eq. (6.29).
                                                           1/2

                                                       2
                                             L      2π CE
                                                 =                              (6.29)
                                             k
                                               D      S y
                      Also shown in Fig. 6.21 is point C, also on the Euler curve, that defines a slenderness
                    ratio, denoted (L/k) C , where the critical stress has been set equal to the yield stress (S y ).
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