Effects of hypersonic speed on the behaviour of normal shocks

[theudster]

TL;DR

What happens to normal shocks at hypersonic speed

I am learning about hypersonic flow now and there seems to be a lot of discussion about the effects on oblique shock as the Mach tends to be very large.
I was wondering what happens to the normal shock as the Mach number tends to be high and I can't seem to find anything about it. Is it because it is not possible to have a normal shock at hypersonic speeds?

 

[.Scott]

I am not precisely clear on your question, but ...
In this image, notice that when shock waves meet, they combine:
Super sonic missile - shock waves (phys.org)

 

[boneh3ad]

You don't find much on it because nothing happens. They still obey all of the same rules they did before, and since they aren't attached to a body, you don't have some of the fun interactions you can get with oblique shocks.

For that matter, so do oblique shocks. The issue is just that oblique shocks tend to get so close to the surfaces generating them that the effect of the boundary layer can no longer be ignored and the inviscid approximation typically used for supersonic flows breaks down. This is called either the viscous-inviscid interaction or the hypersonic viscous interaction.

 

[cjl]

Does anything interesting happen with regards to molecular dissociation actually changing the gas quantity/species through the shock or anything like that, or is the energy still not quite high enough for that?

 

[boneh3ad]

It sure can but it all depends on Mach number and ambient conditions. You can be hypersonics with or without that.