Dassault/Dornier Alpha Jet
grabcad
This is my reinterpretation of the Alpha jet design. I employed NACA 63-212 airfoils on the wings, implementing a twist angle of 2 degrees for optimal aerodynamic performance. For both initial and steady-state operating points, I opted for NACA 0009 airfoils to ensure smooth airflow transitions. Computational fluid dynamics simulations were conducted at an alpha angle of 15 degrees and a velocity of 70 meters per second to validate the design's aerodynamic characteristics.
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