Page 76 - Understanding Flight
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CH03_Anderson  7/25/01  8:56 AM  Page 63




                                                                                                   Wings 63



                                                 2
                      Table 3.1 Typical wing loading (lb/ft )
                                                   Wing Loading
                                                              2
                                                     2
                                Type             (lb/ft )  (kg/m )
                      Sailplane                      6      30
                      General aviation (single engine)  17  85
                      General aviation (twin engine)  26   130
                      Jet fighter                   70     350
                      Jet transport                120     600



                        The reason may be structural considerations. A long slender wing
                      requires more material. A lower aspect ratio wing may save enough on
                      structural weight to offset the reduced lift efficiency, since induced
                      power goes as the load squared. Since weight is probably the
                      singularly most important design criterion, the final wing design must
                      take weight into account. A lighter wing means a lighter airplane and
                      this allows the designer to use a smaller wing area. The smaller wing
                      weighs even less, so there is a cascading positive effect of designing a
                      lighter wing. However, at low speeds the decision to use a low aspect
                      ratio wing will result in higher induced power, so a larger engine
                      might be necessary.
                        Another reason to choose a low aspect ratio wing, despite its
                      inefficiency, may be for aerobatics. A high aspect ratio wing will not
                      roll as quickly as a low aspect ratio wing. In aerobatics the difference
                      in roll rate can be the edge in a competition. The same is true for
                      fighter aircraft. In close combat it is desirable to have a more
                      maneuverable plane than the adversary.
                        In contrast, airplanes that are designed for high-altitude
                      flight, such as the U-2 reconnaissance airplane, have very  A wandering albatross has an
                      high aspect ratio wings, as can be seen in Figure 3.5. At high  aspect ratio of 20, equivalent to
                      altitudes the amount of air available to divert is very small so  a standard-class sailplane, while
                      airplanes must fly at a high angle of attack. In Chapter 2 we  the highly maneuverable
                      discussed that high angles of attack mean greater induced  humming bird has an aspect
                      power. High aspect ratio wings reduce induced power and are  ratio of less than 7. The YF-22
                      the wing of choice for high altitude. A notable exception is the  stealth fighter (Figure 3.36) has
                      SR-71 Blackbird shown in Figure 3.6. But that airplane has  an aspect ratio of 2.4.
                      other performance criteria that set it apart from other high-
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