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9.4 Lift 509<br />

Considerable effort<br />

has gone into reducing<br />

the aerodynamic<br />

drag of automobiles.<br />

numerical calculations. As a result it is possible to predict the aerodynamic drag on cars of a wide<br />

variety of body styles.<br />

As is indicated in Fig. 9.27, the drag coefficient for cars has decreased rather continuously<br />

over the years. This reduction is a result of careful design of the shape and the details 1such as<br />

window molding, rear view mirrors, etc.2. An additional reduction in drag has been accomplished<br />

by a reduction of the projected area. The net result is a considerable increase in the gas mileage,<br />

especially at highway speeds. Considerable additional information about the aerodynamics of<br />

road vehicles can be found in the literature 1Ref. 302.<br />

F l u i d s i n t h e N e w s<br />

At 10,240 mpg it doesn’t cost much to “fill ’er up” Typical<br />

gas consumption for a Formula 1 racer, a sports car, and a sedan<br />

is approximately 2 mpg, 15 mpg, and 30 mpg, respectively.<br />

Thus, just how did the winning entry in the 2002 Shell Eco-<br />

Marathon achieve an incredible 10,240 mpg? To be sure, this<br />

vehicle is not as fast as a Formula 1 racer (although the rules require<br />

it to average at least 15 mph) and it can’t carry as large a<br />

load as your family sedan can (the vehicle has barely enough<br />

room for the driver). However, by using a number of clever<br />

engineering design considerations, this amazing fuel efficiency<br />

was obtained. The type (and number) of tires, the appropriate<br />

engine power and weight, the specific chassis design, and the<br />

design of the body shell are all important and interrelated considerations.<br />

To reduce drag, the aerodynamic shape of the highefficiency<br />

vehicle was given special attention through theoretical<br />

considerations and wind tunnel model testing. The result is<br />

an amazing vehicle that can travel a long distance without hearing<br />

the usual “fill ’er up.” (See Problem 9.90.)<br />

The effect of several important parameters 1shape, Re, Ma, Fr, and roughness2 on the drag coefficient<br />

for various objects has been discussed in this section. As stated previously, drag coefficient<br />

information for a very wide range of objects is available in the literature. Some of this information<br />

is given in Figs. 9.28, 9.29, and 9.30 below for a variety of two- and three-dimensional, natural and<br />

man-made objects. Recall that a drag coefficient of unity is equivalent to the drag produced by the<br />

dynamic pressure acting on an area of size A. That is, d 1 2rU 2 AC D 1 2rU 2 A if C D 1. Typical<br />

nonstreamlined objects have drag coefficients on this order.<br />

9.4 Lift<br />

As is indicated in Section 9.1, any object moving through a <strong>fluid</strong> will experience a net force<br />

of the <strong>fluid</strong> on the object. For objects symmetrical perpendicular to the upstream flow, this force<br />

will be in the direction of the free stream—a drag, d. If the object is not symmetrical 1or if it<br />

does not produce a symmetrical flow field, such as the flow around a rotating sphere2, there<br />

may also be a force normal to the free stream—a lift, l. Considerable effort has been put forth<br />

to understand the various properties of the generation of lift. Some objects, such as an airfoil,<br />

are designed to generate lift. Other objects are designed to reduce the lift generated. For example,<br />

the lift on a car tends to reduce the contact force between the wheels and the ground, causing<br />

reduction in traction and cornering ability. It is desirable to reduce this lift.<br />

9.4.1 Surface Pressure Distribution<br />

The lift can be determined from Eq. 9.2 if the distributions of pressure and wall shear stress around<br />

the entire body are known. As is indicated in Section 9.1, such data are usually not known. Typically,<br />

the lift is given in terms of the lift coefficient,<br />

The lift coefficient<br />

is a dimensionless<br />

form of the lift.<br />

C L <br />

l<br />

1<br />

2rU 2 A<br />

(9.39)

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