Hanley Innovations
VisualFoil NACA
: Airfoil Analysis Software

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VisualFoil NACA


Sale! Buy NACA Version ($29 ). Download Only. Regular price is $69.

Overview

VisualFoil NACA is a modern easy-to-use airfoil analysis and design software for Windows XP, Vista & 7.  The NACA Version is suitable for most users who need to analyze and obtain data for NACA 4, 5, & 6-digit airfoil shapes.

VisualFoil can quickly and inexpensively determine the best cross section shapes for  wings, spoilers, struts, hydrofoils, keels, rudders and other aerodynamic and support structures.

Feature of VisualFoil 5 Include:

  • Export and plot NACA 4, 5 & 6 Digit coordinates in text or .dxf file format.
  • Compute and compare the lift, drag and moments of the NACA 4, 5 and 6 digit airfoil shapes.
  • Built-in library of NACA 4, 5 & 6-digit airfoils
  • Compute and graph  Cl, Cd & Cm versus angle of attack.
  • Stall model to predict the maximum lift coefficient and angle of attack for maximum lift.
  • Built-in graphs
  • Built-in tables
  • Export tables to .csv files
  • Export airfoil to .dxf files
  • Airfoil plotting

Note:  The NACA version of VisualFoil 5.0 does not read-in custom airfoils & .DXF files.  It will analyze and modify NACA 4, 5 & 6-digit airfoils and generate lift, drag and moment coefficients. It can export and plot these airfoil shapes.  The price is only $69. Click Here to Buy NACA Version.

Flow Solver

  • Linear strength vortex panel method
  • Coupled boundary layer solver to compute profile drag.
  • Lift, drag & moment coefficient calculations.
  • Prediction of transition & separation points to demonstrate the validity of your calculations.
  • Stall & maximum lift prediction
  • Surface graphs of pressure  coefficient & velocity ratio for clear explanations of the boundary layer behavior.
  • Beautiful color contour graphs of the pressure coefficient for your reports and presentations.
  • Custom graphs of Cl, Cd & Cm versus angle of attack that you can use in your homework assignments and final reports
  • Multiple graphs of Cl vs Cd for explanining why you picked one airfoil over the other.

Screen Shots

airfoil analysis: drag and stall prediction
VisualFoil can predict profile drag and stall.

airfoil performance comparison
Compare the performance of many airfoils on a single graph.

learn about airfoils in the classroom
VisualFoil is an excellent educational tool for K-12 & beyond.

Video Demo

Purchase

The NACA version (only NACA 4, 5 & 6-digit airfoils) is $69.  Please use the link below to purchase the software.
Program Name/Version Price Purchase Link
Sale! VisualFoil-NACA

$69  $29 US.

Purchase VisualFoil NACA

Share

Purchase
The NACA version (only NACA 4, 5 & 6-digit airfoils) is $69.  Please use the link below to purchase the software.
Program Name/Version Price Purchase Link
Sale! VisualFoil-NACA

$69  $29 US.

Purchase VisualFoil NACA

Computer System Requirements
VisualFoil NACA is a stand-alone airfoil analysis and design software package that requires Windows XP, Vista, Version 7 or 8.

Request More Information:
For more information, please email us at sales@hanleyinnovations.com.

See Also:
MultiElement Airfoils, MultiSurface Aerodynamics, VisualFoil Plus

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