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Modelling and analysis of suspension systems 211 {V G } 1 {V GE } 1 { 2 } 1 {R GE } 1 (4.147) ⎡V ⎢ ⎢ V ⎣⎢ V Gx Gy Gz (4.148) {V H } 1 {V HJ } 1 { 5 } 1 {R HJ } 1 (4.149) 2 ⎡VHx ⎤ ⎡ 0 1.1062 3.881 10 ⎤ ⎡ 0 ⎤ ⎡252.524⎤ ⎢ V ⎥ ⎢ ⎥ ⎢ Hy ⎥ ⎢ 1.1062 0 14.121 ⎢ ⎥ 229 ⎥ ⎢ 112.968 ⎥ mm/s ⎢ ⎥ ⎢ ⎥ ⎣⎢ VHz ⎦⎥ ⎢ 2 ⎣ 3.881 10 14.121 0 ⎥ ⎦ ⎣⎢ 9 ⎦⎥ ⎣⎢ 3219.588 ⎦⎥ (4.150) The velocity vector {V P } 1 is already available. In summary the velocity vectors for the moving points are as follows: T { VC } [ 120.555 435.157 1979.499 ] mm/s 1 T { VD} [ 204.345 112.260 3355.321 ] mm/s 1 T { VG } [0.0 110.394 3373.150] mm/s 1 T { VH } [ 252.524 112.968 3219.588 ] mm/s 1 T { V } [166.468 108.859 3366.0] mm/s P ⎤ ⎡0 0 0 ⎤ ⎡115⎤ ⎡ 0 ⎤ ⎥ ⎢ ⎥ ⎢ ⎥ 0 0 12.266 275 ⎥ ⎢ 110.394 ⎥ mm/s ⎢ ⎥ ⎢ ⎥ ⎢ ⎥ ⎦⎥ ⎣⎢ 0 12. 266 0 ⎦⎥ ⎣⎢ 9 ⎦⎥ ⎣⎢ 3373.150⎦⎥ 1 Having found the velocity {V C } 1 at the bottom of the spring damper unit point C we can now proceed to carry out a separate analysis of the unit to find the sliding component of velocity acting along the axis C–I. For this phase of the analysis we introduce two new bodies, Body 6 and Body 7, to represent the upper and lower part of the damper as shown in Figure 4.71. I Body 6 Body 7 { 6 } 1 A Body 3 B C 7 C 3 C 6 D Fig. 4.71 Modelling the damper unit for a velocity analysis

212 Multibody Systems Approach to Vehicle Dynamics This phase of the analysis can be facilitated by modelling three coincident points, C 3 on Body 3, C 6 on Body 6 and C 7 on Body 7, all located at point C. While points C 3 and C 7 can be considered physical located at point C, point C 6 is a virtual extension of the upper damper as shown in Figure 4.71. The sliding velocity in the damper can then be determined from the relative velocity {V C6C7 } 1 of points C 6 and C 7 . Since C 6 and C 7 are coincident the relative velocity vector can only act along the direction of sliding, axis C–I, allowing us to adopt a scale factor and reduce the number of unknowns: {V C6C7 } 1 f vs {R CI } 1 (4.151) Since I is a fixed point and applying the triangle law of vector addition gives {V C6 } 1 {V C6I } 1 {V C7 } 1 {V C6C7 } 1 (4.152) Note also that since points C 3 and C 7 move together and are physically located at point C we already have the velocity for this boundary condition from the preceding velocity analysis of the double wishbone linkage: { } { } { } (4.153) Combining these last three equations to substitute (4.151) and (4.153) into equation (4.152) gives ⎡120.555⎤ ⎡ 3 ⎤ { VC6 } 1 { VC6 I} ⎢ 435.157 ⎥ f ⎢ vs 9 ⎥ mm/s (4.154) 1 ⎢ ⎥ ⎢ ⎥ ⎣⎢ 1979.499 ⎦⎥ ⎣⎢ 436⎦⎥ As the suspension moves and the strut component rotates it is also clear that as the only degree of freedom between Body 6 and Body 7 is relative sliding motion then { 6 } 1 { 7 } 1 (4.155) The velocity vector {V C6I } 1 can also be defined using {V C6 } 1 {V C6I } 1 { 6 } 1 {R CI } 1 (4.156) ⎡V ⎢ ⎢ V ⎣⎢ V T T T C7 1 C3 1 C 1 V V = V [ 120.555 435.157 1979.499 ] mm/s C6Ix C6Iy C6Iz ⎤ ⎡ 0 ⎥ ⎢ ⎥ ⎢ ⎦⎥ ⎢ ⎣ Equating the expressions for {V C6I } 1 in (4.154) and (4.157) gives ⎡9 z 436 ⎢ ⎢3 z 436 ⎢ ⎣ 3 y 9 6 6y 6 6x 6 6x 0 6z 6y 6z 6x 6y 6x 0 ⎤ ⎡120.555⎤ ⎥ ⎢ ⎥ 435.157 ⎥ ⎢ ⎥ ⎥ ⎦ ⎣⎢ 1979.499 ⎦⎥ ⎤ ⎡ 3 ⎤ ⎡9 436 ⎥ ⎢ ⎥ 9 ⎥ ⎢ 3 436 ⎢ ⎥ ⎢ ⎥ ⎦ ⎣⎢ 436⎦⎥ ⎢ ⎣ 3 9 f vs ⎡ 3 ⎤ ⎢ 9 ⎥ mm/s ⎢ ⎥ ⎣⎢ 436⎦⎥ 6z 6y 6z 6x 6y 6x (4.157) (4.158) Rearranging (4.158) yields three equations that can be used to solve this part of the analysis: Equation 1 3f vs 436 6y 9 6z 120.555 (4.159) ⎤ ⎥ ⎥ ⎥ ⎦ mm/s

212 Multibody Systems Approach to Vehicle Dynamics<br />

This phase of the analysis can be facilitated by modelling three coincident<br />

points, C 3 on Body 3, C 6 on Body 6 and C 7 on Body 7, all located at point<br />

C. While points C 3 and C 7 can be considered physical located at point C,<br />

point C 6 is a virtual extension of the upper damper as shown in Figure 4.71.<br />

The sliding velocity in the damper can then be determined from the relative<br />

velocity {V C6C7 } 1 of points C 6 and C 7 . Since C 6 and C 7 are coincident the<br />

relative velocity vector can only act along the direction of sliding, axis C–I,<br />

allowing us to adopt a scale factor and reduce the number of unknowns:<br />

{V C6C7 } 1 f vs {R CI } 1 (4.151)<br />

Since I is a fixed point and applying the triangle law of vector addition gives<br />

{V C6 } 1 {V C6I } 1 {V C7 } 1 {V C6C7 } 1 (4.152)<br />

Note also that since points C 3 and C 7 move together and are physically<br />

located at point C we already have the velocity for this boundary condition<br />

from the preceding velocity analysis of the double wishbone linkage:<br />

{ } { } { }<br />

(4.153)<br />

Combining these last three equations to substitute (4.151) and (4.153) into<br />

equation (4.152) gives<br />

⎡120.555⎤<br />

⎡ 3 ⎤<br />

{ VC6 } 1<br />

{ VC6<br />

I}<br />

<br />

⎢<br />

435.157<br />

⎥<br />

f<br />

⎢<br />

vs 9<br />

⎥<br />

mm/s<br />

(4.154)<br />

1 ⎢ ⎥ ⎢ ⎥<br />

⎣⎢<br />

1979.499 ⎦⎥<br />

⎣⎢<br />

436⎦⎥<br />

As the suspension moves and the strut component rotates it is also clear<br />

that as the only degree of freedom between Body 6 and Body 7 is relative<br />

sliding motion then<br />

{ 6 } 1 { 7 } 1 (4.155)<br />

The velocity vector {V C6I } 1 can also be defined using<br />

{V C6 } 1 {V C6I } 1 { 6 } 1 {R CI } 1 (4.156)<br />

⎡V<br />

⎢<br />

⎢<br />

V<br />

⎣⎢<br />

V<br />

T<br />

T<br />

T<br />

C7 1 C3 1 C 1<br />

V V = V [ 120.555 435.157 1979.499 ] mm/s<br />

C6Ix<br />

C6Iy<br />

C6Iz<br />

⎤ ⎡ 0<br />

⎥ ⎢<br />

⎥<br />

⎢ <br />

⎦⎥<br />

⎢<br />

⎣<br />

<br />

Equating the expressions for {V C6I } 1 in (4.154) and (4.157) gives<br />

⎡9 z 436<br />

⎢<br />

⎢3 z 436<br />

⎢<br />

⎣<br />

3 y 9<br />

6 6y<br />

6 6x<br />

6 6x<br />

<br />

0<br />

6z<br />

6y<br />

6z<br />

6x<br />

<br />

6y<br />

6x<br />

<br />

<br />

0<br />

⎤ ⎡120.555⎤<br />

⎥<br />

<br />

⎢<br />

⎥ 435.157<br />

⎥<br />

<br />

⎢ ⎥<br />

⎥<br />

⎦ ⎣⎢<br />

1979.499 ⎦⎥<br />

⎤ ⎡ 3 ⎤ ⎡9 436<br />

⎥ ⎢<br />

⎥ 9<br />

⎥ ⎢<br />

3 436<br />

⎢ ⎥ ⎢ <br />

⎥<br />

⎦ ⎣⎢<br />

436⎦⎥<br />

⎢<br />

⎣<br />

3 9<br />

f vs<br />

⎡ 3 ⎤<br />

⎢<br />

9<br />

⎥<br />

mm/s<br />

⎢ ⎥<br />

⎣⎢<br />

436⎦⎥<br />

6z<br />

6y<br />

6z<br />

6x<br />

6y<br />

6x<br />

(4.157)<br />

(4.158)<br />

Rearranging (4.158) yields three equations that can be used to solve this<br />

part of the analysis:<br />

Equation 1 3f vs 436 6y 9 6z 120.555 (4.159)<br />

⎤<br />

⎥<br />

⎥<br />

⎥<br />

⎦<br />

mm/s

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