I'm not saying that 'metal' or 'wood' are better, I'm saying that you need to be specific about the materials you are talking about before you can make comparisons. You also need to undertand that aircraft are designed to withstand known loads, not thrown together with whatever material is available. I'm sure TD know this, and don't need vague generalisations to decide on structural strength modelling and G limits.
Do you have any evidence that the DH Mosquito was designed to lower G-loading standards than similar metal-construction aircraft? If you do, I'd like to see it.
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04-29-2010, 04:32 AM
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