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0 ResultsPitching moment (Cm) analysis of cambered lifting-body fuselage V3 for a Custer channel-wing RC aircraft (MTOW 1.9 kg). V = 15 m/s, Re ≈ 8e5, k-omega SST. Moment reference x = 400 mm (CG candidate). Baseline A/B vs symmetric fuselage planned.
by slilbaekslilbaek
leegunwoo2002 created this project
16 days ago
0 Geometries 0 Meshes 0 Simulation setups 0 ResultsPitching moment (Cm) analysis of cambered lifting-body fuselage V3 for a Custer channel-wing RC aircraft (MTOW 1.9 kg). V = 15 m/s, Re ≈ 8e5, k-omega SST. Moment reference x = 400 mm (CG candidate). Baseline A/B vs symmetric fuselage planned.
