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Standard sedan (saloon) – baseline load paths    C HAPTER 16.2

           16.2.2.4 Free body diagrams and                      Resolving forces horizontally:
           equilibrium equations for each SSS
                                                                P 10 ¼ P 9                            (16.2.12)
           16.2.2.4.1 Transverse floor beam (front) (1)          Similar equations apply for the right-hand panel.
           Resolving forces vertically and by symmetry (loads are
           assumed to be applied symmetrically about the vehicle  16.2.2.4.7 Panel behind the rear seats (9)
           longitudinal centreline):                          Resolving forces vertically and by symmetry:

             P 1 ¼ F =2                            (16.2.3)     P 11 ¼ P 8                            (16.2.13)
                    pf

           16.2.2.4.2 Transverse floor beam (rear) (2)         16.2.2.4.8 Rear parcel shelf (10)
           Resolving forces vertically and by symmetry:       Resolving forces horizontally and by symmetry:
             P 2 ¼ F pr =2                         (16.2.4)     P 12 ¼ P 9                            (16.2.14)


           16.2.2.4.3 Left and right front inner wing panel   16.2.2.4.9 Floor panel (11)
           (3) and (4)                                        Reaction forces P 5 from the inner front wing panels and
           Resolving forces vertically for the left-hand panel:  forces P 10 from the rear quarter panel are applied to this
                                                              SSS. These will not necessarily be equal so additional
             P 3 ¼ R FL   F pt =2                  (16.2.5)   forces P 13 are required acting at the sides which react on
             A similar equation is obtained for the right-hand  the sideframes. It will be assumed these forces act in the
           panel.                                             direction shown in Fig. 16.2-4 although when numerically
             Taking moments about the rear lower corner:      evaluated, these may be negative (i.e. in the opposite
                                                              directions). Resolving forces horizontally:
              4
             P ¼fR FL l 1   F pt ðl 1 þ l pt Þ=2g=h 1  (16.2.6)  2P 13 ¼ 2ðP 10   P 5 Þ               (16.2.15)
             Resolving forces horizontally:
                                                              16.2.2.4.10 Left-hand and right-hand
             P 5 ¼ P 4                             (16.2.7)   sideframes (12) and (13)

                                                              Bothsideframesareloadedidentically. Examining theforces
           16.2.2.4.4 Dash panel (5)                          acting on the sideframes shows that these have already been
           Equal and opposite reaction forces P 3 to those on the  obtained from equations (16.2.3), (16.2.4), (16.2.8),
           wing panels act on this SSS.                       (16.2.9), (16.2.13), (16.2.14) and (16.2.15). However, it is
             Resolving forces vertically and by symmetry:     necessary to check that equilibrium conditions are satisfied
                                                              by applying the equations of statics. Experience has shown
                                                   (16.2.8)
             P 6 ¼ P 3                                        thatitisessentialtomakethisequilibriumcheckaserrorsdo
                                                              occur with the use of the many equations.
           16.2.2.4.5 Front parcel shelf (6)                    Resolving forces vertically:
           Equal and opposite reaction forces P 4 to those on the  P 6   P 1   P 2 þ P 11 ¼ 0         (16.2.16)
           inner wing panels act on this SSS.                   Resolving forces horizontally:
             Resolving forces horizontally and by symmetry:
                                                                P 7 þ P 13   P 12 ¼ 0                 (16.2.17)
             P 7 ¼ P 4                             (16.2.9)
                                                                Moments may be taken about any point but in order to
           16.2.2.4.6 Rear quarter panels (7) and (8)         reduce the algebra it is better to take moments about
                                                              a point where two forces act. For example, take moments
           Resolving vertically for the left-hand panel:
                                                              about the lower corner of the windscreen pillar where
             P 8 ¼ R RL   F =2                    (16.2.10)   P 6 and P 7 act. This simplifies the equation by eliminating
                         l
                                                              two terms.
             Taking moments about the front lower corner:       Moments about the lower corner of the windscreen:

             P 9 ¼fR RL l 2   F ðl 1 þ l 2 Þ=2gh  (16.2.11)     P 1 l 3 þ P 2 l   P 11 l 5   P 12 ðh 2   h 1 Þ¼ 0  (16.2.18)
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