RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia.compute_bwb_moment_of_inertia

compute_bwb_moment_of_inertia

compute_bwb_moment_of_inertia(bwb_wing, center_of_gravity=[[0, 0, 0]])

computes the moment of inertia tensor for a blended wing body about a given center of gravity. Includes the ability to model a wing fuel tank as a condensed wing

Inputs: - Wing - Center of gravity

Outputs: - bwb wing moment of inertia tensor

Properties Used: N/A