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VisualFoil 5.0 Screens  VisualFoil 5.0 for only $229 $49. Buy Now. Ends July 5

Overview
VisualFoil 5.0 is a new easy-to-use software utility that you can use to quickly and inexpensively determine the suitability of airfoil cross section shapes for incorporation in wings, spoilers, struts, rudders and other aerodynamic or support structures. It replaces handbooks, websites and the cost and time associated with finding the right airfoil. The software allows you select efficient shapes during the conceptual design stage of the project and thus eliminate costly mistakes later in the production phase. VisualFoil 5.0 shares the same modern interface as VisualFoil Plus with a built-in airfoil modification tool and the new custom airfoil editor that reads in .dxf files. The software uses the an accurate linear strength vortex panel analysis routines found in VisualFoil version 4.1 and computes lift, profile drag and moment coefficient for isolated airfoil sections. VisualFoil 5.0 generates graphs of Cl & Cm vs angle of attack and Cl vs Cd. VisualFoil 5.0 produces contour plots of pressure coefficient and streamlines. It  has a large library of built-in airfoils which includes NACA 4, 5 & 6-digit airfoils. In addition, the user can enter custom airfoils. They can analyze and modify existing airfoil shapes.

Incompressible Flow Solver

• Linear strength vortex panel method
• Coupled boundary layer solver
• Lift, drag & moment coefficient calculations
• Prediction of transition & separation points
• Stall & maximum lift prediction
• Surface graphs of pressure & velocity ratio
• Contour graphs of Cp
• Graphs of Cl, Cd & Cm versus angle of attack
• Graphs of Cl vs Cd.

Other Features of VisualFoil Plus

• Custom airfoil editor with .DXF file input.  Software reads in line and arc entities.
• Incompressible flow solver using vortex panel method coupled with boundary layer solver
• Built-in library of NACA 4, 5 & 6-digit airfoils
• Custom airfoil analysis
• Computes Cl, Cd & Cm
• Stall Model
• Built-in graphs
• Built-in tables
• Export tables to .csv files
• Export airfoil to .dxf files
• Airfoil plotting

Computer System Requirements
VisualFoil 5.0 is a stand-alone software package that requires Windows 95 or later.  We recommend a pentium based PC running Windows XP.

Purchase

How to Purchase VisualFoil 5.0

Version	Price	Purchase
Single Perpetual Seat	$229 $49	Buy CD Online/Fax Order
Ten Perpetual Seats	$1,895.00	Buy CD Online/Fax Order

Telephone Orders: Please call us at (352) 687-4466 to place your credit card order by telephone.  We can provide you with a download URL & password after the transaction is processed.

Fax Your Orders: Please click here to fax your order. (.pdf order form)

Order by Mail: Click here to order by mail using a check, money order or credit card.

** The leased versions of VisualFoil Plus are identical to the full perpetual version.  Unlike the perpetual version, however, they require an internet connection to enter a username & password.. Note: All prices subject to change without notice.

Request More Information:
For more information, please email us at sales@hanleyinnovations.com.  We can also be reached by telephone at (352) 687-4466. Our mailing address is Hanley Innovations, Attn. VisualFoil Plus, PO Box 831514, Ocala, Fl 34483-1314.

See Also:
MultiElement Airfoils, MultiSurface Aerodynamics, VisualFoil Plus

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