text: weight of the airplane and the horizontal com- 
  ponent of lift be equal to the centrifugal force. 
  Thus, the aircraft in a steady turn develops a 
  lift greater than weight and experiences in- 
  creased stall speeds. 
  Trigonometric 
  
  ‘relationships allow deter- 
  mination of the effect of bank angle on stall 
  speed and load factor. The load factor, B, is 
  the proportion between lift and weight and is 
  determined by: 
  
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              [html]<thead><tr><td>Configuration</td><td>Czmax</td><td>αforCLwar</td></tr></thead><tbody><tr><td>--------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------</td><td>2.</td><td>—</td></tr><tr><td>Clean ( βaps up )...........................................................................................................................................................................................</td><td>1.5</td><td>206</td></tr><tr><td>Maps. down...............................................................................................................................................................................................</td><td>2.0</td><td>18.10</td></tr></tbody>
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