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  • Users: Aerodesign
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  1. Aerodesign

    Ti-3ALv2.5 - stress strain TABLES1 for MATS1 material definition (20 deg C)

    I am working on a landing gear design/stress which is using T1-3ALv2.5 tubing. Linear static analysis indicates higher than yield stresses in various places. I have refined the model to enable believable stresses to be recovered (FE is mixed 1d, 2d and 3d elements) and now need to define the...
  2. Aerodesign

    Tension Fitting (Angle and Channel) understrength mitigation

    This is a question for aero stress engineers. We have a few locations showing negative MS where an external load (modification) is attached to a fuselage through the skin into a new reinforced channel or angle type fitting. The stack-up of parts on the fuselage side consists of skin double...
  3. Aerodesign

    Tension Fittings Filler Pads - Throat Pads - thread2-297984

    Some good work on this thread by edbgtr in 2011, thank you. I am trying to use the calc method for a filler pad on angle and channel tension fittings which have been manufactured undersized. Hence they need throat pads applied - currently tentatively sized based on a nominal efficiency factor...
  4. Aerodesign

    UL bearing allowable in mixed material joints

    I am analysing joints that consist of metallic plates with thermoplastic (TP) skins. The load path uses a metallic plate 1 plus TP skin with load passing to a thicker matallic plate 2. The assumption for bearing is that the ult bearing joint allowable is the metallic plate 1 allowable plus TP...
  5. Aerodesign

    Creep law data for PA66 using Nastran CREEP card

    Members, I am looking for some data covering the generic Pa66 (unfilled) and possibly PA66 (13% GF filled) so that we can do some Nastran creep analysis. The CREEP card in nastran SOL 106 requires a lot of parameter input. The loading situation is RT (20 deg C), constant load for 5yrs (say...
  6. Aerodesign

    Appropriate use of washers in metallic joints

    We have a number of metallic-metallic joints clamping sections of spanwise sub-spar comonents together with spreader plates. Loads are predominently in plane with minimal pull-thru loads (ie in axial direction of the bolts). We do not usually use washers in these joints. Is anyone aware of...
  7. Aerodesign

    CATIA v5 - CatDrawing dimensions

    I am finding that when i Create dimensions on a drawing catia defaults to mm My options-- paramatures and measure units is set to inches My part is created in inches How do I get the dimensions to default to inches
  8. Aerodesign

    SS316L SN - Fatigue data

    We have an assy using a solid 5" bar of 316L with 24" dia x 3/8" thick flanges welded at 18" intervals. I need to look at suitable SN data for 316L but cannot locate any in my available sources. Any ideas where to find data?
  9. Aerodesign

    Patran laminate modeller - multi-layup files

    I have a problem with Patran 2001r2a and laminate modeller. I am making layup files within LM but they are not being saved. I only noticed after making 10 or so files. The Plys are defined in Groups and l have plybooks generated so can re-create the layups OK, but l thought Patran/LM could...

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