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1
0
1 Geometry
1 Mesh
1 Simulation setup
1 ResultR02 only. Sealed fuselage external-flow baseline at 300 km/h (83.333 m/s), zero incidence, air flowing -X toward the +X nose. Excludes arms, motors, propellers, vents and internal hardware. Preliminary steady incompressible k-omega SST study; mesh and convergence validation required before interpreting drag.
by slilbaekslilbaek
jacobo_s_amado created this project
3 days ago
1 Geometry 1 Mesh 1 Simulation setup 1 ResultR02 only. Sealed fuselage external-flow baseline at 300 km/h (83.333 m/s), zero incidence, air flowing -X toward the +X nose. Excludes arms, motors, propellers, vents and internal hardware. Preliminary steady incompressible k-omega SST study; mesh and convergence validation required before interpreting drag.
