Page 58 - Understanding Flight
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CH02_Anderson  7/25/01  8:55 AM  Page 45




                                                                                          How Airplanes Fly 45



                      energy consumed must be minimized. That is, we want to    For maximum lift efficiency one
                      produce the desired lift for the least induced power. Thus  must accelerate a large amount
                      one must make m as large as possible and reduce v to as   of air at as low a velocity as
                      small as possible. For maximum lift efficiency one must   possible.
                      accelerate a large amount of air at as low a velocity as pos-
                      sible. This gives the desired lift with the least energy given
                      to the air.
                        Because the rotors on a helicopter are quite small for the weight of
                      the aircraft, they must accelerate a relatively small amount of air to a
                      high velocity (high kinetic energy) to produce the needed lift. This is
                      inefficient. A similar argument can be made to understand why an
                      airplane cannot  “hang” on its propeller. Although the engine is
                      producing sufficient power to lift the airplane with the wings, the
                      propeller accelerates too little air at too high a velocity to produce the
                      necessary lift on its own. One airplane that can hang on its propellers
                      is the Bell-Boeing V-22 Osprey tilt-rotor aircraft shown in Figure 2.18.
                      The extreme propellers, or  proprotors, divert a great deal of air,
                      allowing the engines to produce enough thrust to lift the craft
                      vertically off the ground before they are rotated forward for
                      horizontal flight.



                        Lift Requires Power
                        Sometimes one encounters the misconception that a wing
                        requires very little power to produce lift and that there is no
                        net downwash behind the wing.This misconception is easy to
                        understand. In many computations in aerodynamics the
                        calculations are done with two-dimensional airfoils.These are
                        in fact infinite wings.This is done because an infinite wing is
                        much easier to calculate than one of finite span.The efficiency
                        of a wing increases with the span of the wing, since the
                        amount of air diverted increases with area.Thus, an infinite
                        wing diverts an infinite amount of air at zero velocity to
                        produce lift, and thus is infinitely efficient.The net vertical
                        velocity of the downwash is zero.Therefore, the infinite wing
                        requires no power to produce lift. Of course, this is not the
                        situation for a real three-dimensional wing.
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