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range of positions investigated the axial force change was minimal ;

                    however, the front axle lift changes dramatically. These data indicate

                    front undernose spoiler fore and aft position is an effective way to vary

                   front axle lift with minimum axial force change.


                         Effect of Vehicle Attitude - Sensitivity of lift and axial force to

                   vehicle attitude is shown in Figure 10 for both the Daytona and the 1969

                   race car. As shown, the axial force and front end lift are very sensi­

                    tive to body attitude and the 1969 race car and the Daytona exhibit

                   very different axial force characteristics as a function of body angle.

                   The 1969 race car achieves minimum drag at-1.5°           body angle whi      the

                   Daytona minimum drag angl      C D  is -.5°. The front axl   c o  lift coefficient,

                   while reduced by about .2 by the Daytona Package,             xhibits a highe d

                                                                      than the 1969 race car.       Rear
                                                                   O
                   sensitivity per degree of body rake angl J
                   axle lift coefficient is relatively insensitive to body attitude. The

                   sensitivity of both configurations illustrates the importance of body

                     ttitude and establishes -.5° as the optimum attitude for the Daytona.
                   C O

                         Effects of Rear Deck Stabilizers - Figure 11 shows the minor axial

                   force panalty resulting from the rear deck stabilizers. At a horizontal

                   stabilizers angle (<Xq)      of -10°, the axial force is increased by 7% at

                   zero yaw angle. Figure       11 also presents the front axle and rear axle

                    lift coefficients as a function of yaw angle. These data indicate the

                   wide range of rear axl       lift coefficients available with the horizontal

                     tabilizer (approximately .14 for       C O  10° change in **g)• Note that as the

                   horizontal stabilizer angl      D  C  H*  c n  increase negatively, the front axl  lift

                   increases slightly. This, of course, is due to the horizontal stabilizer

                   being positioned behind the rear wheels. A more optimum position for

                   the horizontal stabilizer would be directly over the rear wheels.



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