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              [html]<thead><tr><td>Upper to define the effect of density altitude on disruption</td></tr></thead><tbody><tr><td>( 2 ) Gross weight — a large effect on distance.</td></tr><tr><td>Characteristic humidity — to correct take - off distance for the power loss associated with water vapor.</td></tr><tr><td>( 4 ) Wind — a large effect due to the wind or wiid component along the runway.</td></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr><tr></tr></tbody>
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  To obtain minimum landing distance at the 
  specified landing velocity, 
  the forces which 
  act on the airplane must provide maximum 
  deceleration (or negative.acceIeration) during 
  the landing roll. The various forces actin~g. 
  on the airplane during the landing roll may 
  require various techniques to maintain landing 
  deceleration at the peak value. 
  
  Figure 2.34 illustrates the forces acting on 
  the aircraft during landing roll. The power- 
  plant thnrJt should be a minimum positive 