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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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