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In this image we see a normal shockwave in a pipe, the pressure builds at the inlet, and chokes at the throat as the fluid reaches mach 1. We call it choked because the pressure builds up and the pressure terminates in a shockwave, downstream the pressure drops. Along the wall we see as the pipe widens, the pressure drops at the wall, but raises at the center. The pressure at the center is caused by secondary shockwaves by the supersonic flow along the wall reflecting and adding to the drag caused by the primary shockwave. You can see in the first image the expansion fan is weaker and the reflecting compression waves are also weaker leading to a more uniform flow downstream.

The bottom image where the normal shock is strongest has the strongest compression waves from the expansion fans, creating in effect a constriction in a supersonic flow. In compressible/trans/super sonic flows constrictions raise pressure and slow down airflow. It is only after the bulk airflow passes this constriction that the overall pipe pressure decreases. Had the wall been constructed more carefully, one could largely avoid the compression waves while maintaining the expansion fans that further accelerate a choked flow. This would reduce losses substantially.

In the bottom image if you look closely you can see the recirculation bubble.

In this image we see a normal shockwave in a pipe, the pressure builds at the inlet, and chokes at the throat as the fluid reaches mach 1. We call it choked because the pressure builds up and the pressure terminates in a shockwave, downstream the pressure drops. Along the wall we see as the pipe widens, the pressure drops at the wall, but raises at the center. The pressure at the center is caused by secondary shockwaves by the supersonic flow along the wall reflecting and adding to the drag caused by the primary shockwave. You can see in the first image the expansion fan is weaker and the reflecting compression waves are also weaker leading to a more uniform flow downstream. The bottom image where the normal shock is strongest has the strongest compression waves from the expansion fans, creating in effect a constriction in a supersonic flow. In compressible/trans/super sonic flows constrictions raise pressure and slow down airflow. It is only after the bulk airflow passes this constriction that the overall pipe pressure decreases. Had the wall been constructed more carefully, one could largely avoid the compression waves while maintaining the expansion fans that further accelerate a choked flow. This would reduce losses substantially. In the bottom image if you look closely you can see the recirculation bubble.

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[–] • 1 pt

Strakes to create vortices on the inside of the wheels. I discovered a way to improve aero performance by doing something that looks stupid on the surface. Most aero is focused to getting air around the outside of the wheels, using air screens to reduce turbulence. I went to the inside of the wheel instead, by combining wheel alignment, and strakes, I'm directing air so that it outwashes into the inside of the tire along the brake ducts. I learned via experiments that if you toe out a spinning wheel it creates a strong jetting vortex, so I guide airflow along the inside of the wheel, along with suspension aligment so the wheel sees basically airflow at a 15-20 degree angle depending on where the front wheels are pointing. I don't have as much freedom in the back, but doing this took out all the understeer at the front of the car. I had to weld brackets to the chassis to keep the upper control arms from being ripped off the chassis. I did this on 200 tread wear tires, you need to run slicks to get that kind of loading, so I know I'm on to something.

[–] • 0 pt

Nice. That is definitely something. Doesn’t matter what it looks like, liquid physics is weird stuff, just that the end sum of traction and drag is less.