Dear All,

I've been trying to use A320 B8 (1
PV Elite
-20 - 100F 18.8ksi
to 200F 18.8ksi
to 300F 16.7ksi

I checked it in ASME as well but it seems different to me.
ASME:
-20 - 100F 18.8ksi
to 200F 16.7ksi
to 300F 16.3ksi

Can anyone help? Maybe it's just me not understanding something.
I'd need the stress value at 150F
Thanks


Attachments
821-A320_B8_1_t_1_1_4.JPG


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Regards,
Istvan