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1 Geometry
3 Meshes
1 Simulation setup
0 ResultsThis project focuses on the baseline external aerodynamic analysis of a Gulfstream II business jet without winglets. The objective is to study airflow around the complete aircraft and evaluate lift, drag, pressure distribution, and velocity distribution. The results will serve as a baseline for comparison with a modified aircraft configuration featuring a morphing trailing edge.
Yuvitha created this project
3 days ago
1 Geometry 3 Meshes 1 Simulation setup 0 ResultsThis project focuses on the baseline external aerodynamic analysis of a Gulfstream II business jet without winglets. The objective is to study airflow around the complete aircraft and evaluate lift, drag, pressure distribution, and velocity distribution. The results will serve as a baseline for comparison with a modified aircraft configuration featuring a morphing trailing edge.
by slilbaekslilbaek
