[NSRCA-discussion] Elevator trim change

Mon May 8 16:59:11 AKDT 2006

Gray, do you think the CTE of the AeroSlave laminate would be different than the styrofoam laminate used by many others?
  ----- Original Message ----- 
  From: Gray E Fowler 
  To: NSRCA Mailing List 
  Sent: Monday, May 08, 2006 10:51 AM
  Subject: Re: [NSRCA-discussion] Elevator trim change


  Fiberglass laminate CTE = 6 X10 -6/in/in/F 

  CF pushrod CTE = 1 X 10 -6 /in/in/F  ....could actually be 0 if fiber vloume is > 58% an all uni fibers 


  Gray Fowler
  Principal Chemical Engineer
  Composites Engineering


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