[NSRCA-discussion] Elevator trim change

Gray E Fowler gfowler at raytheon.com
Mon May 8 07:52:43 AKDT 2006


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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