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Thread: Allowable Nozzle Loads

  1. #13

    nozzle laods spreadsheet

    plz email me spreadsheet at engr_shaharyar@hotmail.com

    thanks in advance

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  3. #14
    Please send spread sheet to me on engrtm@hotmail.com

    Thank you,

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  5. Please send me the spread sheet to recrajesh@yahoo.co.in
    Thanks,

  6. #16
    Hi,
    Please also send me the excel spreadsheet for Nozzle load calculations on my mail ID prasenjitd@in.dclgroup.co.in
    All the best for you!!

  7. Hi
    Please also send me the excel spreadsheet for Nozzle load calculations on my mail ID farzam.fathi@gmail.com

    Thznks in advance

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  9. please send my email id also.i am also expecting that one>it is usefulr for me for enrich my knowlege rrajakumar79@gmail.com

  10. Hi Carlos,

    kindly send me the Excel Spreadsheet too. My mail address is raja687@hotmail.com

    Regards

  11. #20
    Hy,
    Please also send me the excel spreadsheet for Nozzle load calculations on my mail ID da7onediva@yahoo.com
    All the best for you!!
    __________________

  12. 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.

  13. 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! tableA2=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

  14. Hi,
    Please also send me the excel spreadsheet for Nozzle load calculations on my mail ID vikascha123@yahoo.co.in
    thanks

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  16. #24

    nozzle load

    plz send nozzle load calculation spread sheet
    my mail id dhinas2003@yahoo.com

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