voko said:
As I said earlier, a conical shock wave is an idealization where the supersonic body is assumed to have been supersonic forever. It is the product of the interference of the spherical shock waves excited by the body continuously during its infinite flight.
I am talking about the case when a subsonic body becomes supersonic and the shock wave system forms for the first time. The first, so to speak, spherical shock wave has nothing to interfere with in the rear hemisphere, so it will propagate as a spherical shock there.
I am not commenting the rest of your message because you are obviously talking about a different regime.
The problem is that your assumption here about the nature of shocks is incorrect. The conical shock is not an idealization that requires the supersonic body to have been supersonic forever. Decades of schlieren and shadowgraph images have shown conical and other oblique shocks forming on surfaces that get accelerated from stationary to supersonic and it still forms an oblique shock.
A subsonic body becoming supersonic is no different. It is simply a time-varying system, but the shock ultimately comes from the same source. The body, even when subsonic, is essentially sending information about itself through tiny pressure/density waves that radiate away from the body continuously. In a subsonic flow, these waves are still there but propagate fast enough that a given wave is never caught by its subsequent waves (or at least not before significant amounts of dissipation has occurred). As you speed up, the waves on the front side are emitted closer together than they were until eventually they get so close that they start to interact with the waves emitted before them. This is when compressibility starts to become important in the flow.
Once you reach the speed of sound, these waves can no longer get out of the way of the ones emitted subsequently and the resulting finite-amplitude waves "break" and become a shock wave. This shock wave becomes increasingly oblique as the velocity continues to increase. Wikipedia actually has a very nice set of animations showing this based on a point source that emits a series of discrete waves.
Stationary ([itex]M=0[/itex]):
Subsonic ([itex]M<1[/itex]):
Sonic ([itex]M=1[/itex]):
Supersonic ([itex]M>1[/itex]):
where [itex]M[/itex] is the Mach number.
There is never and will never be a shock wave in the rear of the moving point source, as those waves are not actually "piling up". On a more realistic shape like a diamond, there is a shock at the rear because the air leaves the surface at a nonzero angle relative to the free stream and must be turned back in line with the free stream. Usually this turning involves compression, and information about the compression cannot propagate upstream since it is traveling faster than the speed of sound, so a shock must accomplish the compression and flow turning.
There is no discontinuity that forms solely as a result of a body accelerating past the speed of sound. If and when a discontinuity does form, it is a result of the supersonic compression required behind the body. At exactly [itex]M=1[/itex], the "weak" shock would be spherical, but it would quickly dissipate, as it isn't really a shock, but on the cusp of forming a shock, and it would be spherical in the sense that its "front end" would be located at the rear of the object and the center would be at the location where the object started.