Page 84 - Understanding Flight
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CH03_Anderson  7/25/01  8:56 AM  Page 71




                                                                                                   Wings 71



                      root stalls. If the tip stalled first, the pilot would lose roll con-  Philanthropist Daniel Guggenheim
                      trol during the stall. This could lead to an uncontrolled stall-  was an aviation enthusiast. The
                      spin. If wings are designed such that the root stalls first, the  Daniel Guggenheim Fund
                      pilot can control the airplane and prevent the spin.      established seven aeronautical
                        Though  mechanically twisting the wing is common on     schools in the late 1920s. These
                      general-aviation aircraft, commercial transports and other high-  were MIT, Caltech, University of
                      performance airplanes use an aerodynamic twist. Aerodynamic  Michigan, NYU, Stanford, Georgia
                      twist results when the wing sections are changed from root to tip.  School of Technology (now
                      In other words, different wing section designs are selected for  Georgia Tech), and the University
                      different positions along the span of the wing. For example, a  of Washington. Of the seven
                      designer might reduce the camber of the wing sections from root  original, only NYU no longer has
                      to tip. The goal is to select a wing that is more lightly loaded at  a program in aeronautics.
                      the tip and will not stall at the same angle that the wing root
                      stalls. The result is that the wing behaves as though it is twisted,
                      although it is twisted aerodynamically and not mechanically.


                      Wing Configuration

                      There is still more to a wing than its airfoil and planform. The config-
                      uration of the wing, as viewed from the front, can affect stability, effi-
                      ciency, and practicality. Why are wings sometimes slanted up or down
                      from the root to the wingtip? Should the airplane have a low wing, a
                      high wing, or a midwing? What type of wingtip is best? When should
                      one consider a biplane?

                      Dihedral
                      Roll and yaw stability are desirable characteristics for trainers and trans-
                      ports, both of which can be enhanced by adding dihedral to the wings.
                      Dihedral is the upward angle of the wing along the span against the
                      horizon, as shown in Figure 3.14. Many are taught that the reason dihe-
                      dral adds stability is that as the airplane rolls gravity pulls the
                                                                                Manfred Von Richthofen (the Red
                      upward wing back to horizontal. Unfortunately, the truth is
                                                                                Baron) flew the Fokker triplane,
                      more complex.
                                                                                for which he is famous, for only
                        When an airplane enters a roll, there is a tendency to yaw
                                                                                6 weeks and 19 of his 80
                      in the opposite direction. For example, if the airplane rolls to
                                                                                victories.
                      the right, it is accompanied by a yaw to the left. That is, the
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