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Old 20th Aug 2017, 17:56
  #39 (permalink)  
tmmorris
 
Join Date: Feb 2003
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Originally Posted by Genghis the Engineer
I'd second that - flexibility is a major part of how aircraft structures handle loads - a very rigid structure will suffer much higher transient stresses under variable load than a flexible one.
If you ever get the chance to be on top of a church tower while the bells are ringing you'll find it flexes. Rather alarming the first time...
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