RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.generate_fuseform_vortex_distribution

generate_fuseform_vortex_distribution

generate_fuseform_vortex_distribution(VD, fus, n_cw, n_sw, spc, precision)

This generates the vortex distribution points on a fuselage or nacelle component Assumptions: If nacelle has segments defined, the mean width and height of the nacelle is used Source: None

Inputs: VD - vortex distribution

Properties Used: N/A