RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_fuselage.compute_fuselage_fineness#
- compute_fuselage_fineness(fuselage, x_locs, eff_diams, eff_diam_gradients_fwd)[source]#
This computes fuselage finenesses for nose and tail.
Assumptions: Written for OpenVSP 3.16.1
Source: N/A
Inputs: 0. Pre-loaded VSP vehicle in memory, via import_vsp_vehicle. 1. RCAIDE fuselage [object]. 2. Array of x_locations of fuselage segments. (length = L) 3. Array of effective diameters of fuselage segments. (length = L) 4. Array of effective diameter gradients from nose to tail. (length = L-1)
Outputs: Writes fineness values to RCAIDE fuselage, returns fuselage.
Properties Used: N/A