text: The typical airflow patterns exemplify the 
  relationship of static pressure and velocity 
  defined by Bernoulli. Any object placed in an 
  airstream will have the a& to impact or stag- 
  nate at some point near the leading edge. The 
  pressure at this point of stagnation will be an 
  absolute static pressure equal to the total pres- 
  sure of the airstream. 
  In other words, the 
  static pressure at the stagnation point will be 
  greater than the atmospheric pressure by the 
  amount of the dynamic pressure of the air- 
  stream. As the 
  flow divides and proceeds 
  around. the object, the increases in local ve- 
  locity produce decreases in static pressure. 
  This procedure of flow is best illustrated by the 
  flow patterns and pressure distributions of 
  figure 1.7. 
  
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              [html]<thead><tr><tdcolspan="2">Table</td></tr></thead><tbody><tr><td>Patients</td><td>Paltitude density ratio, ρ / p0</td></tr><tr><td>Table</td><td>Sult</td></tr><tr><td>The TAS is a function</td><td>0</td></tr></tbody>
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