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  • Users: no2metal
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  1. no2metal

    Unbalanced layup

    Is composite wing mainly of quasi layup construction? and is it only for the only skins or the stiffeners like spars, ribs and stringers. I came across a presentation mentioning using unbalanced layup on the wing design to overcome the twisting, is this just simply add on extra plies on a quasi...
  2. no2metal

    Pull strength

    Gents, Can pullout strength (e.g. of an insert or bolt)of composite be determined by analysis??
  3. no2metal

    Backout factors

    Does anyone has any info on using Backout factors in calculating UD (0 degree) lamina property from crossply (0/90) laminate Thanks in advance

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