WebVSP

WebVSP

Geom Browser

Geom Editor

General

Name

Display

Mode

Tessellation

Num W

Color

Wire

Material

Preset

Ambient

Diffuse

Specular

Emitted

Alpha

Shininess

Transforms

X Loc

Y Loc

Z Loc

X Rot

Y Rot

Z Rot

Rot Origin X

Scale

Symmetry

Planar

XY XZ YZ

Axial

None X Y Z

Axial N

Volume-Based Mass Properties

Density

Priority

OML-Based Mass Properties

Include Thin Shell

Mass/Area

Specified Mass Properties

Mass

X CG

Y CG

Z CG

Ixx

Iyy

Izz

Ixy

Ixz

Iyz

Computed Mass Properties

Total Mass

Volume

Area

Design

Length

Length

Breadth

Height

Height

Diameter

Diameter

A Radius

B Radius

C Radius

Length

Fine Ratio

Spine

Width

Height

Shape

Airfoil Cross Section

Chord

T/C

Camber

Camber Loc

Invert Airfoil

Diameter

Angle

Modeling

Prop Mode

Design

Diameter

Num Blades

Cylindrical Foils

Reverse

Rotate

Use Beta 3/4

Beta 3/4

Feather

Pre-cone

Construct X/C

Feather Axis

Feather Offset

Prop / Rotor Metrics

Activity Factor

-

r0

CLi

-

C/R

-

C_T/R

-

C_P/R

-

Solidity

-

Solidity T

-

Solidity P

-

Blade

Curve

Curve Type

Shift, Rotate, & Scale

Delta X/C

Delta Y/C

Theta

Scale

Shift LE

Fold Axis

Angle

Radial/R

Axial/R

Offset/R

Azimuth

Elevation

Units

Length Unit

Mass Unit

Anthropometric

Gender

Stature

Stature %

BMI

BMI %

Mass

Volume

Auto Density

Age

Sitting H / H

Show Skeleton

Pose

Preset

R/L Sym

Body

Back

Waist

Head

Nod

Rotate

Right Side

Arm

Shoulder AB/AD

Shoulder FE

Shoulder IE

Elbow

Forearm

Wrist

Leg

Hip AB/AD

Hip FE

Knee

Ankle

Left Side

Arm

Shoulder AB/AD

Shoulder FE

Shoulder IE

Elbow

Forearm

Wrist

Leg

Hip AB/AD

Hip FE

Knee

Ankle

Planform

Span

Root Chord

Tip Chord

Sweep (LE)

Dihedral

Twist

Twist Loc

Taper

-

Area

-

Sections

Wing Section

Section

Name

Num Sections

-

Interpolated XSecs

Num U

Section Planform

Projected Span

-

Area

-

AR

-

Taper

-

Ave C

-

Span

Root Chord

Tip Chord

Sweep

Sweep

Sweep Loc

Sec SW Loc

Twist

Twist

Twist Loc

Dihedral

Dihedral

XSec

Section

Name

Num XSecs

-

Location

X Loc

Y Loc

Z Loc

Interpolated XSecs

Num U

Shape

Type

Size

Width

Height

Thickness

Camber

Camber Loc

Sharp TE

Thick Loc

LE Radius Index

Six Series

Six Series A

Wedge Camber

Flat Up

Wedge Symmetric

Thick X Low

Flat Low

VKT Epsilon

VKT Kappa

VKT Tau

Upper Degree

Lower Degree

CST Upper

CST Lower

Max Width Loc

Corner Radius

Top Tan Angle

Bottom Tan Angle

Top Strength

Bottom Strength

Upper Strength

Lower Strength

Fuse File

Choose File

Name

-

Curve Type

Cockpit Side

Exponent

Corner Radius

Airfoil File

Choose File

Name

-

Prop Sections

Section

Name

Num Sections

-

Location

Radius

Num U

Airfoil

Type

Camber

Camber Loc

Sharp TE

Thick Loc

LE Radius Index

Six Series

Six Series A

Wedge Camber

Flat Up

Wedge Symmetric

Thick X Low

Flat Low

VKT Epsilon

VKT Kappa

VKT Tau

Upper Degree

Lower Degree

CST Upper

CST Lower

Max Width Loc

Corner Radius

Top Tan Angle

Bottom Tan Angle

Top Strength

Bottom Strength

Upper Strength

Lower Strength

Fuse File

Choose File

Name

-

Curve Type

Cockpit Side

Exponent

Corner Radius

Airfoil File

Choose File

Name

-

Thickness

Skinning

Airfoil

Section

Type

Camber

Camber Loc

Sharp TE

Thick Loc

LE Radius Index

Six Series

Six Series A

Wedge Camber

Flat Up

Wedge Symmetric

Thick X Low

Flat Low

VKT Epsilon

VKT Kappa

VKT Tau

Upper Degree

Lower Degree

CST Upper

CST Lower

Max Width Loc

Corner Radius

Top Tan Angle

Bottom Tan Angle

Top Strength

Bottom Strength

Upper Strength

Lower Strength

Fuse File

Choose File

Name

-

Curve Type

Cockpit Side

Exponent

Corner Radius

Airfoil File

Choose File

Name

-

Thickness

Image

Texture

Choose File

Name

-

Keep aspect ratio

Size

Width

Height

Rename Geometry