I wonder if you guys know, that braising was the preferred method of joining chrome molly for years. From the time they started manufacturing different chrome molly in the 40s threw the 50s all your F1 cars and WW2 aircraft where braised and held up very well. There was no real problem till mass manufacturing needed a faster way to join them. The fact is you can weld them with a torch, FAA still approves this method on experimental aircraft. You can Mig and you can Tig even though NHRA won't let you Mig. Excessive heat is the culprit that weakens joints. Your heat settings rod or wire, how the joint fits and how fast you travel with your rod all enter in to a good weld. If you have any doubts about your weld, first look at the heat ring by the weld. If it extends more than the width of the weld, you may be too hot, too slow or using wrong rod or wire. Then cut a couple apart and see if your bead goes to the bottom of the joint. If the bead on the bottom of the joint is more than about 1/3 the width of the top, you may be too hot. If you see a line of the joint your too cold. If it was easy everyone would be willie the welder. I don't care for joining dissimilar metals especially if the wall thickness is different, but it can be done well. It just taxes your ability to direct the heat more. The Tig is a little easier to control the heat and run, but a good welder with an oxy acct torch can do it also and not impossible with a Mig. Beating a joint to test strength is probably not as effective as pulling them apart with your frame machine. Tensile strength is where they most likely fail. One other tip. Make sure your CM is of the normalized variety. usually has a N at the end of the number. This should not have to be annealed after a proper weld.
I'm not a chassis builder but I stayed in a Holiday Inn once.
I'm not a chassis builder but I stayed in a Holiday Inn once.
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