Page 56 - Understanding Flight
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CH02_Anderson  7/25/01  8:55 AM  Page 43




                                                                                          How Airplanes Fly 43



                      may wonder how the design of the wing affects the induced power
                      requirements. In other words, what is the wing’s efficiency for lift?
                        Efficiency for lift has to do with the amount of induced power it
                      takes to produce a certain lift. The lower the induced power needed
                      the greater the efficiency. The most obvious way to improve
                      the efficiency of a wing is to increase the amount of air
                                                                                Approximately 600 million people
                      diverted by the wing. If more air is diverted, the vertical
                                                                                fly on domestic commercial
                      velocity of the air is reduced for the same lift and so is the
                                                                                routes per year. That’s over 1.6
                      induced power. This is accomplished by increasing the size of
                                                                                million a day!
                      the wing.
                        Another important contribution to the induced power requirements
                      of a wing is the additional loading due to the upwash. In brief, the
                      upwash puts an additional load on the wing on the order of 20 percent
                      of the lift for a general-aviation airplane. This additional load
                      decreases with increasing aspect ratio. This is discussed in the section
                      on ground effect.
                        In consideration of the total efficiency of a wing, the parasitic power
                      (or parasitic drag) must also be considered. The parasitic power of a
                      wing is proportional to its area. So for cruise speeds where parasitic
                      power dominates there is a limit to how much the area of the wing can
                      be increased to reduce the induced power. There are additional
                      problems with increasing the wing’s area, particularly by making it
                      longer. The first is that large wings are heavy and increase the weight
                      of the airplane. The second is that long wings are not as structurally
                      strong as shorter wings. If two wings have the same area, the longer
                      one will be the most efficient due to reduced upwash loading, though
                      it will be weaker. Gliders operate at speeds where induced power
                      dominates. Thus the high-performance gliders have long
                      wings. Figure 2.17 shows a glider with a 60:1 glide ratio. This
                                                                                Sea birds, which must fly long
                      means that in still air, the glider travels 60 ft horizontally for
                                                                                distances without landing, also
                      every foot it descends to provide power. It is interesting to note
                                                                                have high aspect ratio wings for
                      that sea birds, which must fly long distances without landing,
                                                                                optimum efficiency.
                      also have high aspect ratio wings for optimum efficiency.
                        Most fast airplanes have shorter wings. An exception is the U-2 spy
                      plane, which flew at 460 mi/h (740 km/h) above 55,000 ft (16,700 m).
                      The U-2 had long wings because of the extreme altitudes at which it
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