Page 24 - Understanding Flight
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CH01_Anderson PFS2  7/25/01  8:55 AM  Page 11





                                                                                             Basic Concepts  11



                      is measured (P  in the figure). In the situation in the figure,
                                   total                                        Alexander Graham Bell was a
                      P   is the same at both points A and B. In the language of  founding member of the Aerial
                       total
                      pilots, this is also known as the Pitot pressure, and the figure  Experiment Association (AEA),
                      illustrates a Pitot tube.                                 which was organized to try to
                        The second pressure to consider is the  static pressure  be the first in flight. It was
                      (P   ), which is measured perpendicular to the airflow    disbanded in 1908 but had been
                        static
                      through a hole in the wall. This is the pressure most often  partially successful with the
                      referred to when the air pressure is discussed in         designs of Glenn Curtiss.
                      aerodynamics. In the figure the static pressure is higher at
                      point A than at point B.
                        The third pressure is the dynamic pressure (P  ), which is the
                                                                   dynamic
                      pressure due to the motion of the air, and is a pressure parallel to the
                      flow of air. The dynamic pressure is proportional to the kinetic energy
                      in the air. Thus the faster the air goes the higher the dynamic pressure.
                      This may seem a little complicated, so let us try to put it all together.
                        The total pressure  P   is the sum of the static and dynamic
                                            total
                      pressures (P   and P      ). We have shown how to measure the
                                 static    dynamic
                      total, or Pitot, pressure and the static pressure. How is the dynamic
                      pressure of the air measured? Look at the setup in Figure 1.10.
                      Between the tube that measures the total pressure and the tube that
                      measures the static pressure there is placed a differential pressure
                      gauge. That is a gauge that measures the difference in pressure
                      between the two ports, which is the difference between total and
                      static pressure. Since static plus dynamic pressure is equal to total
                      pressure, this difference between total and static pressures is the
                      dynamic pressure.
                        If no energy is added to the air (by some mechanism such as a
                      propeller) the total pressure remains the same and an increase in
                      dynamic pressure causes a decrease in static pressure. So when one
                      reads that the pressure of air decreases because it is going faster, the
                      pressure referred to is the static pressure. But what if energy is added to
                      the air? In the right-hand corner of Figure 1.9 is the picture of a fan.
                      What has happened to the air pressures at point C? The fan is
                      accelerating the air, and thus has done work on the air. Thus the
                      dynamic pressure has increased. Since the air is not confined, the static
                      pressure is the same as in the surrounding environment and thus has
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