Answer:
The thrust is  [tex]F = 7828.3 \  N [/tex]
Explanation:
From the question we are told that
  The speed of the jet aircraft is  [tex]v = 214 \ m/s[/tex]
  The rate at which the engine takes in air is [tex]\^ Q = 115 \ kg/s[/tex]
  The rate  at which the engine burns fuel is  [tex]\r m = 2.53 \ kg/s[/tex]
  The speed of the exhaust gases is  [tex]u = 276 \ m/s[/tex]
 Â
Generally the thrust of the engine is mathematically represented as
   [tex]F =[ \^ Q * ( u - v )] + (\r m * u)[/tex]
=> Â [tex]F =[ 115 * ( 276 Â - Â 214 )] Â + (2.53 * 276)[/tex]
=> Â [tex]F = 7828.3 \ Â N [/tex]