Page 53 - Understanding Flight
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CH02_Anderson  7/25/01  8:55 AM  Page 40




                 40  CHAPTER TWO



                                       tional to the lift of the wings times the vertical velocity of the down-
                                       wash. Now if we were to double the load, maintaining the same
                                       speed, we would have to double the vertical velocity of the air to
                                       provide the necessary lift. Both the load and the vertical velocity of
                                       the air have been doubled and the induced power has gone up by a
                                       factor of 4. Thus, the induced power increases as the load squared.
                                       It is easy to see why the weight of an airplane and its cargo is so
                                       important. Figure 2.15 shows the data for the relative fuel con-
                                       sumption of a heavy commercial jet as a function of weight. These
                                       measurements were made at a fixed speed. From the data one can
                                       estimate that at a gross weight of 500,000 lb (227,000 kg) and a
                                       speed of Mach 0.6 about 40 percent of the power consumption is
                                       induced power and 60 percent is parasitic power. In reality the air-
                                       plane would cruise at a speed of around Mach 0.8, where the
                                       induced power would be lower and the parasitic power consump-
                                              tion would be higher. Unfortunately, at that more realistic
                                              speed the details of the power consumption become more
                    The induced power increases as
                                              complicated and it is more difficult to separate the parasitic
                    the load squared.
                                              and induced powers from the data.



                                           1.6
                                                            Fuel Consumption vs. Load


                                           1.4
                                         Fuel Flow (arb. units)  1.2







                                           1.0
                                                                           Constant Speed
                                                                           Mach 0.6

                                           0.8
                                               300       350      400        450       500      550
                                                                 Gross Weight (x 1000 lb)
                                       Fig. 2.15. Fuel consumption vs. weight for large jet at a constant speed.
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