Page 72 - Understanding Flight
P. 72

CH03_Anderson  7/25/01  8:56 AM  Page 59




                                                                                                   Wings 59



                        A thicker wing will have a structural advantage, since the  The Fokker D-VII was the first
                      wing’s structure can be contained inside the wing itself. The  airplane to exploit thick wings.
                      thin wings used by early airplanes required external bracing  As a result it was the only
                      and thus higher parasitic drag. Before aerodynamic drag was  airplane specifically mentioned in
                      understood toward the end of WWI, emphasis was placed on  the Treaty of Versailles. The
                      thin wings, with many wires and struts to give the wing   Germans were required to hand
                      strength. Biplanes were used most frequently because they  over every airplane to the Allies.
                      made for a nice boxlike structure. There is a natural
                      competition between the aerodynamicist who wishes to have a thin
                      wing and the structural engineer who wants the wing to look
                      internally like a nice fat box.

                      Leading Edge

                      Another design characteristic to be considered in designing a wing is
                      the shape of the leading edge. A wing with a sharp leading edge will
                      go abruptly into a stall. A blunt leading edge will have a much less
                      abrupt stall entry, with the stall starting at the trailing edge with the
                      separation point progressing forward as the stall becomes deeper. Fig-
                      ure 3.1 shows the early stall development of a wing with a well-
                      rounded leading edge as well as the stall of a wing with a sharp
                      leading edge. The wing with the sharp leading edge goes directly into
                      a full stall. Another way of looking at stall entry is shown in Figure
                      3.2, which shows the lift as a function of effective angle of attack for
                      both wings. It is clear that the sharp wing goes from maximum lift to
                      full stall with a very small change in angle of attack.
                        Airplanes that are designed to operate at lower speeds or to be used
                      as trainers have fairly round leading edges. Fast jet fighters have
                      sharper leading edges. A difficult problem for pilots transitioning from
                      lower-speed trainers to high-speed fighters is appreciating the more
                      abrupt stall. Many new pilots have been “surprised” when their high-
                      speed airplane stalled without warning. A classic use of a sharp
                      leading edge wing section is on the F-104 Star Fighter, shown in Figure
                      3.3. The leading edge is so sharp it has been known to cut the hands
                      of mechanics who inadvertently rub against it.
                        STOL (short takeoff and landing) aircraft have very fat, round
                      leading edges. This will hurt the airplanes’ top cruise speed, but top
   67   68   69   70   71   72   73   74   75   76   77