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Supersonic Flow Simulation Setup by mithun is a document available to read on EtoBox.
What is Supersonic Flow Simulation Setup about?
The document describes a simulation setup to analyze supersonic flow around an aircraft engine intake. It details the geometry, mesh, boundary conditions, and material properties used. The results show contour plots of pressure, temperature, and Mach number around the intake. There is a 386924 Pa total pressure loss across the engine inlet. Adding a 3mm insulating layer with low thermal conductivity (0.1 W/mK) reduces the maximum engine temperature from 463.292 K to 422.864 K, showing the insulating effect.
- Author
- mithun
- Language
- EN