Table of Contents

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Getting Started
Definitions

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File
Open
Import
Drawing Interchange (.dxf)
x, y, z Data
Create
NACA 4 and 5 digit
NACA 6 and 7 Series
Oshkosh
Inverse Design
Save
Airfoil Coordinates
Drawing Interchange (.dxf)
Results
Image

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Edit
Control Surface Modeling
Mean Line Modification
Coordinate Spacing
Surface Smoothing

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View
Surface Velocity
Pressure Coefficient vs Surface
Pressure Coefficient vs Chord
Boundary Layer Thickness
Gamma
Alpha Plot
Drag Polar
Surface Velocity vs Chord
Tabulated data

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Tools
Multiple Airfoils
Show Airfoil Coordinates
Graphic Options
Rename Airfoil
Angle of Attack Range

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Options
Inviscid
Viscous
Reynolds Number
Constant Lift
Wing Simulation
Compressibility
Surface Conditions

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Help
Registration

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Single User License