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No Stress Peaks

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Apsu

Apsu

Aerospace
Joined
Dec 30, 2010
Messages
10
Location
GB
Does any one know of a method to design a gas turbine or compressor blade so that under a combined tension (CF) and gas bending load the traditional located stress peaks at LE,TE and Blade to Platform are avoided.
 
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pls don't simultaneous post in different forums
 
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