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types.md

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CurrentModule = VortexStepMethod

Enumerations

Model
WingType
AeroModel
PanelDistribution
InitialGammaDistribution
SolverStatus

Basic Vectors

MVec3
PosVector
VelVector

Aerodynamic data

AeroData

Wing Geometry, Panel and Aerodynamics

A body is constructed of one or more abstract wings. All wings are of type Wing. A Wing has one or more sections and can be created from YAML files or OBJ geometry.

Section
Section(LE_point::PosVector, TE_point::PosVector, aero_model)
Wing
Wing(n_panels::Int; spanwise_distribution::PanelDistribution=LINEAR,
     spanwise_direction::PosVector=MVec3([0.0, 1.0, 0.0]))
ObjWing
ObjWing(obj_path, dat_path; alpha=0.0, crease_frac=0.75, wind_vel=10., mass=1.0,
         n_panels=54, n_sections=n_panels+1, spanwise_distribution=UNCHANGED,
         spanwise_direction=[0.0, 1.0, 0.0])
BodyAerodynamics

The Solver and its results

Solver
VSMSolution