Supersonic flow in a rocket nozzle
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- เผยแพร่เมื่อ 25 ส.ค. 2024
- Visualization of pressure, wall-pressure, vorticity and velocity fields durind the start-up of a rocket nozzle. We can notice the transition between a Free Shock Separation (FSS) configuration and a Restricted Shock Separation (RSS) configuration with the increasing of the pressure ratio. This simulation was performed at the CORIA laboratory with the CHOC WAVES code.
Hello, would yoiu be willng to share a working file of this demo?
The algorithm sent this video to you too?
@@SPVLaboratories hi, I was actually looking at very similar stuff to this for a while now hahha, so my algo is already loaded with similiar machine visions thingies