wes616
Aerospace
- Mar 19, 2005
- 940
Thought I'd post this here before heading home for the day. Any ideas about defining an explicit formula for kerfing nomex panels. Right now our shop does this process by trial and error, but we need to determine something more explicit than this quality purposes. I can't seem to come up with anything that will work (beyond trial and error approximations)...
Does anyone know of a formula (or a place to find a formula) that will relate the kerfing cuts to bend radius. (or am i just forgetting some basic geometry here)?
Wes C.
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When they broke open molecules, they found they were only stuffed with atoms. But when they broke open atoms, they found them stuffed with explosions...
Does anyone know of a formula (or a place to find a formula) that will relate the kerfing cuts to bend radius. (or am i just forgetting some basic geometry here)?
Wes C.
------------------------------
When they broke open molecules, they found they were only stuffed with atoms. But when they broke open atoms, they found them stuffed with explosions...