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Thread: G load with Pitch Rate
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Old 11th Feb 2021, 12:18
  #10 (permalink)  
DaveReidUK
 
Join Date: Jan 2008
Location: Reading, UK
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Originally Posted by FlightDetent
Just saying that if G could be determined directly from TAS and pitch rate, it would need to be solely dependent on those two variables. Rubbish.
In fact those two parameters are neither necessary nor sufficient.
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