Page 131 - Understanding Flight
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CH05_Anderson  7/25/01  8:58 AM  Page 118





                 118  CHAPTER FIVE



                                       It’s Newton Again


                                       You learned in Chapter 2 that for a wing to create lift it must divert air
                                       down. This principle is exactly how an aircraft propulsion system
                                       works, except that to create thrust it must push air back. Just as your
                                       household fan pushes air back, so does a propeller and a jet engine. For-
                                       tunately, your house fan does not have enough thrust to propel itself.
                                         Also like wings, aircraft propulsion systems are applications of
                                       Newton’s laws. Remember Newton’s third law states that “for every
                                              action, there is an equal and opposite reaction.” In an aircraft
                    Harriet Quimby was the first U.S.
                                              propulsion system, the action is acceleration of air or exhaust
                    woman to earn a pilot certificate
                                              and the reaction is the force, or thrust, produced. Again we
                    and in 1911 was the first
                                              use the alternate form of Newton’s second law which states
                    woman to cross the English
                                              that the thrust is proportional to the amount of gas accelerated
                    Channel.
                                              per time times the speed of that air.

                                       Thrust


                                       Though it is not an aircraft propulsion system as such, studying the
                                       rocket engine is an excellent way to understand propulsion. An exam-
                                       ple of how a rocket engine works is shown in Figure 5.1. Fuel and an
                                       oxidizer are pumped into a combustion chamber, producing a large
                                       amount of gas at a high pressure. The gas accelerates to the throat of
                                       the motor, where it reaches a velocity of Mach 1. After the throat the


                                       Oxidizer



                                                               Throat
                                                   Combustion
                                                   chamber                 Nozzle     High-velocity gas






                                            Fuel
                                       Fig. 5.1. Schematic of a rocket engine.
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