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Old 20th December 2012 | 15:32
  #199 (permalink)  
clkorm3
 
Joined: Nov 2008
Posts: 47
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From: Land of Hope
can someone please tell me how this is worked out.

Question: If an aeroplane performs a steady co-ordinated horizontal turn at a TAS of 200 kt and a turn radius of 2000 m, the load factor (n) will be approximately: 1.1.

Many thanks
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