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Thread: Allowable Nozzle Loads

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  1. I was make excell spreadsheet ) i need just read the diagram value, and my excell table can be found the result, but i have a problem! I testing that for the example calculation (in the WRC107 buletin, appendix), and I can't calculate the correct value of four raw so, my excell table is not correct yet, pls help me somebody! so, my problems is the following:
    WRC107, page 65, tableA1=correct! tableA3=correct TABLEA3, incorrect! problems: vessel and nozzle section, longitudinal and transverse plane, inner surface! the other value is correct in my calculation. If somebody know, whitch is the correct equtation for above raw, pls send me! turitamas84@gmail.com thank you in advance


    "that was in the past"
    Last edited by tturit; 04-03-2010 at 07:50 PM.

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