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LH2/LOx Combustion Chamber CFD Analysis by Đinh Quốc Trí is a document available to read on EtoBox.
What is LH2/LOx Combustion Chamber CFD Analysis about?
The document summarizes a computational fluid dynamics (CFD) simulation of a liquid rocket combustion chamber using liquid hydrogen and liquid oxygen propellants. The simulation was performed using the Ansys FLUENT software. The geometry and meshing were done in GAMBIT. The study varied parameters like the number of inlets for better mixing and nozzle designs to attain high exhaust velocity and impulse. Previous work on liquid hydrogen/liquid oxygen rocket engines and combustion is also reviewed. Key findin
- Author
- Đinh Quốc Trí
- Language
- EN