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Standard sedan (saloon) – baseline load paths    C HAPTER 16.2
                                                                X
                          θ A             θ C                      F VERTICAL ¼ 0.   Q 2 þ Q 3 VERTICAL

                    Q 3V                                                         Q 5 VERTICAL þ Q 6 ¼ 0
                H    B       Q 3H             E  Q 5H
                                 G
                                        Z
                   h 1                        Q 5V  h 2
                                                              16.2.3.6 Some notes on the standard
                            X                                 sedan in torsion
                                     L 5                      (a) A knowledge of the shear stress s in the panels is
                                                              required. The panel thickness t must be chosen so that
           Fig. 16.2-15 Components of forces Q 3 and Q 5 .    shear stress is within permitted values. The average shear
                                                              stress s in the continuous shear panels can be calculated
                                                              from the edge force Q by:
             They can then be solved using a standard computer
                                                                          Q
           method (e.g. Gaussian reduction) available widely. Most  s AV ¼
           ‘spreadsheet’ programs can do this. To ensure reliability   shear area
           of the solution, the matrix should be ‘positive definite’.  The force intensity on a panel edge is often expressed
           This requires all terms on the leading diagonal of the  as shear force per unit length or ‘shear flow’ q. Shear flow
           coefficient matrix to be positive and non-zero, and this is  is related to shear stress thus q ¼ ts. As with shear stress
           the reason for the rearrangement of the order in which  systems, every shear flow has an equal ‘complementary’
           the equations are listed.                          shear flow q at 90 to it.
                                                                        0

             Solution of the equations gives values for the edge  For example in the roof (see Fig. 16.2-12):
           forces Q 1 to Q 7 .                                  Shear flow on front of roof q 1 ¼ Q 1 /B. Shear flow on
             The stresses in the shear panels and ring frames  side of roof q 4 ¼ Q 4 /L 7 but the latter would be the
           can then be estimated.                             complementary shear flow to q 1 . From equation (16.2.23)
                                                              above:
           16.2.3.5.1 Solution check                            Q 1 L 7 ¼ Q B
                                                                          4
           It is easy to make errors in the setting up of the equi-  hence, substituting:
           librium equations. The solution for edge forces Q should
           be checked to ensure force balance in both horizontal and  ðq 1 BÞL 7 ¼ðq L 7 ÞB
                                                                            4
           vertical directions on the sideframe. Referring to Figures
           16.2-14 and 16.2-15:                               thus
             X
                F HORIZONTAL  ¼ 0.Q 3 HORIZONTAL  þ Q 4         q 1 ¼ q ðcomplementary shear flowsÞ
                                                                      4
                               þ Q 5 HORIZONTAL    Q 7   Q X1   For a car of constant width B such as this one, the
                                                              shear flows q 1 on panel edges across the car are all the
                                 Q X2 ¼ 0
                                                              same at q 1 ¼ Q 1 /B. For the panels subject to edge



            Table 16.2-1 (b)
            Force (Figure 16.2-15)     Component         Moment about G        Moment arm about G

                                       Q 3 sinðq A Þ     ðh 1  ZÞQ 3 sinðq A Þ  r 3H ¼ðh 1  ZÞ
            Q 3H
                                       Q 3 cosðq A Þ     ðXÞQ 3 cosðq A Þ      r 3V ¼ðXÞ
            Q 3V
                                       Q 5 sinðq C Þ     ðh 2  ZÞQ 5 sinðq C Þ  r 5H ¼ðh 2  ZÞ
            Q 5H
            Q 5V                       Q 5 cosðq C Þ     ðL 5  XÞQ 5 cosðq C Þ  r 5V ¼ðL 5  XÞ
            Force                             Moment about G                          Moment arm about G

                                       Q 3 fðh 1  ZÞ sinðq A ÞþX cosðq A Þg    r 3 ¼ðh 1  ZÞ sinðq A ÞþX cosðq A Þ
            Q 3
                                       Q 5 fðh 2  ZÞ sinðq C ÞþðL 5  XÞ cosðq C Þg  r 5 ¼ðh 2  ZÞ sinðq C ÞþðL 5  XÞ cosðq C Þ
            Q 5


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