David Martin
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- Joined
- Apr 7, 2008
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Expounding on Desoto's last 2 sentences. Through strenuous test the military found that aluminum aircraft parts (think frame, i.e. spar) would flex under G force at max. gross and power. Climbing and fast decent. The character of aluminum is to flex SOME then return to it's original line. If flexed too much it did not return. But instead developed Stress, leading to a stress fracture. i.e. failure. Whereas the wood laminate did not show this conduct. Thus, it was deemed stronger. DM