Index

_

__init__() (aerodemo.naca_airfoil.NACAFiveDigit method) (aerodemo.naca_airfoil.NACAFourDigit method) (aerodemo.vlm.VortexLatticeMethod method) (aerodemo.vlm.WingGeometry method)

A

add_fuselage() (in module aerodemo.openvsp_utils) add_horizontal_tail() (in module aerodemo.openvsp_utils) add_vertical_tail() (in module aerodemo.openvsp_utils) add_wing() (in module aerodemo.openvsp_utils) aerodemo.naca_airfoil module

aerodemo.openvsp_utils module aerodemo.vlm module aspect_ratio (aerodemo.vlm.WingGeometry property)

C

camber_line() (aerodemo.naca_airfoil.NACAFiveDigit method) (aerodemo.naca_airfoil.NACAFourDigit method) check_openvsp() (in module aerodemo.openvsp_utils)

cl() (aerodemo.naca_airfoil.NACAFourDigit method) coordinates() (aerodemo.naca_airfoil.NACAFiveDigit method) (aerodemo.naca_airfoil.NACAFourDigit method)

D

dihedral (aerodemo.vlm.WingGeometry attribute)

I

init_vsp() (in module aerodemo.openvsp_utils)

L

lift_curve_slope() (aerodemo.naca_airfoil.NACAFourDigit method)

load_vsp3_file() (in module aerodemo.openvsp_utils)

M

max_camber (aerodemo.naca_airfoil.NACAFourDigit property) max_camber_location (aerodemo.naca_airfoil.NACAFourDigit property) max_thickness (aerodemo.naca_airfoil.NACAFiveDigit property) (aerodemo.naca_airfoil.NACAFourDigit property)

mean_aerodynamic_chord (aerodemo.vlm.WingGeometry property) module aerodemo.naca_airfoil aerodemo.openvsp_utils aerodemo.vlm

N

n_chordwise (aerodemo.vlm.WingGeometry attribute) n_spanwise (aerodemo.vlm.WingGeometry attribute)

NACAFiveDigit (class in aerodemo.naca_airfoil) NACAFourDigit (class in aerodemo.naca_airfoil)

R

reference_area (aerodemo.vlm.WingGeometry property)

root_chord (aerodemo.vlm.WingGeometry attribute) run_vspaero() (in module aerodemo.openvsp_utils)

S

save_vsp3_file() (in module aerodemo.openvsp_utils) solve() (aerodemo.vlm.VortexLatticeMethod method)

span (aerodemo.vlm.WingGeometry attribute) sweep_alpha() (aerodemo.vlm.VortexLatticeMethod method) sweep_angle (aerodemo.vlm.WingGeometry attribute)

T

taper_ratio (aerodemo.vlm.WingGeometry property) thickness() (aerodemo.naca_airfoil.NACAFiveDigit method) (aerodemo.naca_airfoil.NACAFourDigit method)

tip_chord (aerodemo.vlm.WingGeometry attribute) twist (aerodemo.vlm.WingGeometry attribute)

V

VortexLatticeMethod (class in aerodemo.vlm)

W

WingGeometry (class in aerodemo.vlm)

Z

zero_lift_angle() (aerodemo.naca_airfoil.NACAFourDigit method)