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Bad idea - The Blanik wing skin alloy is the same soviet era material
used on early MIG's. Not even close to 2024, probably stronger than 7075-T6, and anodized, not clad. Assuming you can identify the major alloying elements of the factory skins, how will you determine the aging tempering process used, and show compliance/conformance with the design material properties as required by the FAR's? Do you think the factory will give you all the design allowables for this material? Or perhaps you will develop your own per Mil-Hnbk-5? See if you can get a piece from a scrapped ship, I know someone that has several. Aerodyne |
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