Page 107 - Understanding Flight
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CH03_Anderson  7/25/01  8:56 AM  Page 94




                 94  CHAPTER THREE



                                       Wrapping It Up


                                       Before moving to the next chapter discussing stability and control, let
                                       us look at some typical wings and identify what choices were made in
                                       designing them. We will look at the following three airplanes: the
                                       Cessna 172 from general aviation, the Boeing 777 from commercial
                                       aviation, and the Lockheed-Martin/Boeing F22 stealth fighter from the
                                       military.
                                         The Cessna 172, shown in Figure 3.10, is a popular four-seat
                                       airplane with a cruise speed of 120 knots. The wing is unswept but
                                       has a small amount of taper toward the tip. The wing is mounted at
                                       the top of the fuselage for stability and for structural reasons. The
                                       wing has an aspect ratio of 7.5, dihedral for stability, hinged flaps for
                                       landing, and round leading edges for a gentle stall. The low wing
                                       loading gives it good low-speed performance, but its top speed is not
                                       particularly noteworthy. The airplane is designed to be easy to fly and
                                       sports the best safety record of all general-aviation aircraft.
                                         The Boeing 777 (Figure 3.35) is designed to carry a heavy load over
                                       long distances, its high cruise speed, about Mach 0.84, requiring a high
                                       wing loading. The aspect ratio is similar to that of the Cessna 172, but
                                       the wing is swept and tapered. In this case the sweep is necessary for
                                       the high cruise speed. Taper, plus changes in wing section, result in a
                                       roughly elliptic lift distribution at cruise. For takeoff and landing, the
                                       airplane has double-slotted trailing-edge flaps and deployable leading-
                                       edge slats. The wing is fairly thick (a person can stand in the wing
                                       root) to accommodate the necessary structure and fuel. The wing also
                                       has significant dihedral for stability.
                                         The Lockheed-Martin/Boeing F-22 is the current generation stealth
                                       fighter (Figure 3.36). The body and wing blend together for stealth. As
                                       a result it shares the characteristics of a low-wing and a midwing
                                       design. The wing is more highly swept and tapered than the Boeing
                                       777. It is highly maneuverable and can cruise at speeds greater than
                                       the sound speed. The F-22 employs many high-lift devices, including
                                       diverting engine thrust down. Its wing loading is high and it has a
                                       very small aspect ratio.
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