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  1. alex2000junio

    Aircraft Loads Simplification

    I'm working on my final college project on composite materials and studying one of the standard models provided by NASA CRM. I'll be conducting a buckling study in FEMAP on the upper wing surface. To do this, I first need to apply the loads. For the loads, I'm doing the following: I'll consider...
  2. alex2000junio

    FEMAP Static Analyses + Temperature

    Hello, guys! I'm trying to add a temperature to my structural model and combine it with other loads. However, when I do this, FEMAP can't run the analyses. It says temperature loads are not supported in Static Analyses. How am I gonna do this? Are there a way to apply temperature loads to my...
  3. alex2000junio

    AISC 360-22 - Single Angles

    Hello everyone, I'm kind of confused with AISC 360-22 and the design examples. I'd like to know, regarding single angles, when to use the principal axis and when to use the geometric axis (mostly in the Chapter F10). It seems like to me that we should always use the principal axis for all of...
  4. alex2000junio

    Design Guide 9 Calculations

    Another very quick question: Thanks a lottt Bulb the Builder! I really appreciate you help :)
  5. alex2000junio

    Design Guide 9 Calculations

    Hello guys, I have some quick questions about the examples of Design Guide 9 that are not 100% clear to me. - Why does V_u, in example 5.1, is divided by 2? Example 5.4 does not divide. - In Example 5.1, both τ_bw and τ_bf uses Vu. Shouldn't it be V_y for the web one and "V_x divided by 2" for...

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