text: v, p 
  C‘ 
  - 
  -= 
  C %n.*0 V 
  
  The example airplane was specified to have: 
  
  Weight = 14,250 lbs. 
  
  C L,,,=lS 
  
  V,= 100 knots EAS 
  
  table depicts the lift coefficients 
  The following 
  and angles of attack at various airspeeds in 
  steady flight. 