I put this in another thread - I'll try it here and see what happens.
Nothing happens to a bullet when it's velocity changes from sonic to subsonic, or subsonic to sonic. There is no "shock wave" effect. All that takes place is a change in the slope of the curve that describes the effect of wind. It's like you were climbing a hill, when you come to a place that the hill becomes steeper, or less steep, it simply becomes harder ,or easier to climb the hill. I'll go out on a limb here and say bullets might be described as "going very gently" into or out of the transonic region!
I'm sure there will be many who think they could almost hear their bullet hitting a wall in this terrible region called "transonic". Truth is it's difficult to pin point exactly where this region is. Probably it can only be done mathematically and somewhat arbitrarily.
OK pacecil..... I'm only conversant with supersonic flight phenomena but I CAN read, and I DO have real books written by real ballisticians at my disposal so's I refuse to just let'cher allegation lie
As you no doubt know, it's more than just a "steeper slope," the transonic area. And why you're presenting it a "gentle" I dunno but tests agree with theory here, it's not.
Quote for me ONE real ballistics text, show me ONE opinion other than your own or otherwise substantiate your position
else'twise I'll have to give it the same credence as your last exposition wherein you asserted that "smoke rings don't exist because you pointed your airhose around the shop and nothing untoward happened."
According to (Rinker/McCoy/Litz/Vaughn et al) there most certainly IS a shockwave, this shockwave is illustrated/described (verbally/dramatically/photographically) in EVERY ballistics text with which I'm conversant. And all texts agree that in that region where the bullet is "crossing over" it's strongly "buffeted" (this is the most common descriptor) due to the fact that as it ascends/descends through this region there's a period of "back-and-forth" action where parts of the system are protruding or mixing between the two states of flight.
To quote Robt Rinker, 'Understanding Firearm Ballistics, Basic To Advanced Ballistics Simplified & Explained,' "a lot of phenomena occur during this transonic range. Most of the difficulties are associated with shock wave induced flow and pressure changes."
He goes on for pages (with pixtures) explaining/showing how airflow transitions from laminar to "behind the shock wave" with a little "NOTE: Shock waves are different than airflow" accompanying the pixtures.......
In fact Rinker goes so far as to say that "for the study of aerodynamics and airflow at velocities below the speed of sound, air is termed incompressible. At the higher speeds there are large and important changes in air density and compressibility."
Much reference to "turbulence" and "pressure changes moving in all directions...."
sooooo, more input? Something more than just "nothing!"
I've got no answers, no real understanding of laminar airflow flight characteristics, but I hesitate to let your assertion go unchallenged. Wouldn't be prudent.
Good luck
al
(BTW, the (nonexistent) "shock wave effect" as you so indelicately put it is rawther well and easily
explained in ALL of the ballistic tomes on my bookshelf....)