
How can a diverging section after a converging section accelerate the fluid at hypersonic speeds if its speed was sonic at the converging section?
How can a diverging section after a converging section accelerate the fluid at hypersonic speeds if its speed was sonic at the converging section?
A De Laval Nozzle works on that same principle and that is why I am trying to understand it. We can increase the flow speed of a subsonic fluid by decreasing the area in which it flows. When it becomes sonic (its speed gets Mach 1) decreasing the area will not result in a higher speed but a lower rate of mass flow. This occurs because the pressure waves travel too at the speed of sound. But then adding a diverging section can increase its speed above Mach 1. How is that? Some may explain it by saying that the diverging section makes the fluid flow in the direction we want it to, others by saying that the fluid pushes itself of the walls of the diverging section. Generally we can find many explanations online but which one is actually true? Or is there another one which is what really happens and therefore true? We can see in the image a De Laval Nozzle.
"What is happening with Reddit tho, I tried to make this post ffour times before and it was removed by its filters. I tried to add an image and a link to it of a De Laval Nozzle but this might be the issue. At first I tried making the link non-clickable and then not even add an image but it did not seem to work and even making the link non-clickable again. Anyways I provided the image" -Nick Pap