Not to sound condescending because I do appreciate your feedback, but I am a full time machinist and gunsmith. I know what muzzle brakes are, I know what porting is and I know how hard it is to drill a barrel. Forget I ever said drill the barrel. I was trying to simplify this for people who don't know much about guns.
I just wanted an answer as it pertained to nozzles. Weather it is a gun barrel or not does not matter. It can be a pipe and I am trying to make a The picture is of a muzzle brake that was made many years ago and never mass produced. It was designed by a retired propulsion or rocket engineer, who is now passed on.
The brake does everything it is supposed to do. It takes a 55 Ft lb recoil impulse and lowers it to around 13.5 Ft. Lbs. It does not blow hot gas in the shooters face and I am not worried about a dust trail from prone position shooting. I am merely interested in trying to duplicate what he did. He used a "de Laval nozzle" to increase the thrust pressure to make it greater than that of a simple cylindrical hole like in a typical port or brake design. I am asking about the two different throat styles because modern machining a through hole into a cylinder at a 30 deg angle can only be done two ways. The drawings I supplied show the two possible outcomes for what the throats would look like after they were machined.
Since an actual CD Nozzle is not possible because there is no access to machine the convergent section at the combustion chamber, I am guessing that his design is more a Divergent only chamber. So, if it is a divergent chamber, what would make it more efficient, the triangular throat produced by drilling and milling with the form tool and bit at 30 deg like in the triangular cross section, or drill the throat hole at a 90 Deg, and then use the form tool at 30deg. so that you get the throat walls even?
I guess what it all comes down to is If you were going to build it what would you do?