If using special steel alloy ,I´d use 1.7734.4/5 (15CDV6) ,which is readily available in tube flat/sheets and welding rod and is a a bit tougher /improved tensile strength compared to 4130 plus has the advantage of being easier in terms of treatment required before and after welding.Welding is easier if I remeber correctly(haven´t done any welding on 25CrMo4 for a couple of years now ,so maybe
I glorify the weldability of 1.7734 a bit).
Still all very very expensive stuff ...so basically out of range for this kind of project if you are really seriously counting the cost.Ordering two m² sheet metall and a handful of tubes and bar stock result in unbelievable sums( for me).
riff_raff wrote:n smikle,
"UTS of 4340 = 100ksi.. Sn = 50ksi...Safety factor of 4 so design stress = 12.5 Ksi"
I just noted in your previous post that you are using strength values for 4340 alloy steel. 4340 is not readily available in tube form, and is difficult to weld due to its higher carbon content. If your A-arms are welded alloy steel tube, you should probably be using the normalized values for 4130 alloy steel, plus some appropriate Kt knockdown value (stress concentration factor) for analysis of your weld joints.
And of course, this also assumes that your welder is using the correct alloy welding rod, that there is no weld porosity or undercutting, that you properly stress relieve the parts after welding, and that you perform a proper mag particle inspection of the welded and stress relieved parts.
Normalized, air melt DOM 4130 steel tube has a UTS of about 95 KSI, and an elongation rate of about 8%. 4130 responds to heat treatment, so you can get a higher UTS by using a quench and temper cycle. But the thermal quench cycle of your finished weldment would likely produce a substantial amount of distortion, so I would not recommend attempting it.
Regards,