I've tested similar competitor fittings and found most of them cracked. There was one brass fitting that didn't crack, but it was cast and much thicker than mine. The other ones that didn't crack were bronze-brass, but that costs three times as much. One design that preformed well was thicker, so I'm looking into using a larger hex bar to start with (1/16” larger).
Last night I came up with an idea to change the amount of thread engagement. I figured that the more engagement on the threads, the more the stress would be distributed. I then read in Machinery’s Handbook 26 Ed. “It is recognized that in special applications, such as flanges for high-pressure work, longer thread engagement is used, in which case the pitch diameter E1 is maintained and the pitch diameter E0 at the end of the pipe is proportionately smaller.” Basically what it is saying is to change the pitch between the end of the pipe and the plane of hand tight engagement. Has anyone done this, or know how much I should proportionally change the pitch?
As far as hydrogen embrittlement, I don’t think that’s the case. Everything I read about it has to do with steel, or aluminum, or electroplating. I’m sure that SCC caused the cracking in these fittings, which come from a combination of internal stress and exposure to ammonia. I’m waiting for some chrome plated fittings to come in so I can test them for SCC, but I’m concerned by the way contractors might handle the parts, which could scratch off the chrome, leaving the brass exposed.
Anyway, I’ll have to make up a bunch of different designs and test them. Thanks for the help with the stress-strain equation Rich.