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Goof

Kasutaja: Goof

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Structural Testing Of Homebuilt Aircraft
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Structural Testing Of Homebuilt Aircraft

9 17.8 7.5 4.6 ments on each side of the wing. If the 6 29.1 26,0 21.5 15.7 5.3 2.4 wing has been properly constructed and if the designer did not goof, the TAPER 0.1 10 30.1 26.4 21.3 15.1 4.9 2.2 wing should easily support this total 20 31.1 26.6 21 14.4 4.7 2.1 load and will, upon the removal of the ELLIPSE 25.5 24

Mehaanika → Abimehanismid
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