I wish it was that simple... But hopefully UM has a nice fishbone diagram going.
The correlation between what you calculate/simulate and the real world is the worse for bolted joints than anything else I have done in engineering.
I don't know UM's design philosophy, but I can tell you what happens at OEM's. All those calculations/simulations/rules of thumb happen to just get you in the ballpark. Then you test statistically significant number (a ton) of samples with load cells; using production intent fasteners/coatings, Production intent thread form/process, production intent threaded material. Now you iterate the design and testing, but hopefully not too many times.
This is because tiny differences are a big deal here. When you start getting to the fastener to the proof load that's required to keep a properly designed joint together, almost all your applied torque is going to friction. Tiny differences in thread form (class, tapped/rolled, etc.), alloy of the thread material, alloy of the under head material, surface finish of the under head and threads, cleanliness, coatings, paint, etc.
Here is a great case in point, many years ago most grade 8 bolts were Cad plated. There was an industry switch to zinc plating's, that was an absolute disaster for some joints, requiring redesign/new processes, and totally inconsequential to others.