plz email me spreadsheet at engr_shaharyar@hotmail.com
thanks in advance
plz email me spreadsheet at engr_shaharyar@hotmail.com
thanks in advance
Please send spread sheet to me on engrtm@hotmail.com
Thank you,
Please send me the spread sheet to recrajesh@yahoo.co.in
Thanks,
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!!
Hi
Please also send me the excel spreadsheet for Nozzle load calculations on my mail ID farzam.fathi@gmail.com
Thznks in advance
please send my email id also.i am also expecting that one>it is usefulr for me for enrich my knowlege rrajakumar79@gmail.com
Hi Carlos,
kindly send me the Excel Spreadsheet too. My mail address is raja687@hotmail.com
Regards
Hy,
Please also send me the excel spreadsheet for Nozzle load calculations on my mail ID da7onediva@yahoo.com
All the best for you!!
__________________
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.
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
Hi,
Please also send me the excel spreadsheet for Nozzle load calculations on my mail ID vikascha123@yahoo.co.in
thanks
plz send nozzle load calculation spread sheet
my mail id dhinas2003@yahoo.com
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