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AlphaJet_CFD
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1 Geometry
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1 Geometry 0 Meshes 0 Simulation setups 0 ResultsAbout this project
This project aims to simulate the aerodynamic behavior of an Alpha Jet wing profile in compressible flow conditions. The objective is to analyze pressure distribution, velocity fields, and aerodynamic coefficients (Cl, Cd, Cm) at different Mach numbers, particularly in subsonic and transonic regimes. The simulation will be performed using external aerodynamic analysis with a compressible flow model. Results will help understand shock formation and performance variations of the airfoil.
