Hanley Innovations
Keel & Rudder Analysis
Home About Us
Products
Airfoils
Wings
Graphing
eBooks

Contact
Dr. P. Hanley
Tel:(352) 687-4466
PO Box 831514
Ocala, FL 34483

Keel & Rudder Analysis

Tapered Keel Analysis & Design
Compare Span, Airfoils, Sweep & Taper with a 3DFoil Analysis

It is well known that without a keel to provide lateral resistance to the sail side-force, a sailboat cannot travel up-wind.  It is also well know that high performance sailboat races are often decided by a matter of minutes or seconds. Two objectives of a good keel design are (1) to provide enough sideforce resistance (required for powerful sails) and (2) to reduce the unwanted drag component that impedes the boats forward motion. In the past, predicting the performance of new designs meant using a technical manual (similar to this one) to determine the hydrodynamic properties.  A major problem with this approach (other than the obvious time consuming  & error prone table manipulation and manual calculations) is the restriction of the design to know cross section shapes and sailing conditions. 3DFoil  was developed by Patrick Hanley, Ph.D. to provide reliable hydrodynamic data for new appendage designs for any cross section shape and sailing conditions. 3DFoil also generates the planform shape of tapered keels & rudders and provides the airfoil data needed to fabricate the cross sections. With the reliable analysis found in 3DFoil, you will be able to design a custom keel based your custom specifications in a short period of time.

3DFoil Advantages

3DFoil has the following advantages:

  • It replaces the tables, graphs and other (look-up) sources of  hydrodynamic data and allows the designer to instantly compute sideforce and drag for their new design given shape, airfoil and sailing conditions.  The calculations are performed in seconds on the PC instead of hours of error-prone hand calculations.

  • It provides airfoil and 3D keel/rudder analysis which saves hours over airfoil-only software that requires the designer to transport the airfoil data to the actual 3D keel design.

  • 3DFoil replaces first-generation lofting-only software that provides just the airfoil and wing shape data but no analysis to predict the performance of the design. 3DFoil produces .dxf files of cross-sections & a .STL file of the actual full-sized 3-D keel which the designer can prototype directly using a CNC machine.

3DFoil Features

Use 3DFoil's airfoil analysis tools to:

  • Compute lift, profile drag and moment coefficient for airfoil sections.

  • Estimate the maximum lift for airfoil sections at different Reynolds Numbers.

  • Generate multiple graphs of Cl vs. AOA,  Cm vs AOA, Cl vs. Cd, Cl/Cd vs. AOA, etc. to facilitate comparison of airfoil sections at various sailing conditions.

  • Edit, print, copy to clipboard and export graphs to .bmp file format.

  • Generate coordinates for NACA 4, 5 & 6-Digit Airfoils.

  • Read-in custom airfoils sections for analysis (Full Version Only).

  • Modify & save airfoils using the Airfoil Data Tool.

  • Plot airfoils to any size.

  • Export airfoils to .dxf files for inclusion in CAD programs.

To size the actual keel, use the 3DFoil planform design & analysis features to:

  • Compute the overall lift for rectangular & tapered keels & rudders.
  • Analyze the effects of different aspect ratios.
  • Estimate maximum lift for the keels.
  • Compute & compare the profile and induced drag for different keels & rudders.
  • Analyze keels & rudders with distinct airfoils at the root and tip chords (linear aerodynamic twist)
  • Analyze keels with positive/negative dihedral angles for canting keel designs.
  • Analyze keels with forward and backwards sweep to test stability.
  • Compute neutral point for the keels and determine longitudinal stability.
  • Generate graphs and compare CL vs. AOA, CM vs. AOA, CL/CD vs. AOA & CL vs. CD for similar keel and rudder designs.
  • Edit, print, copy to clipboard and export graphs to .bmp file format.
  • Generate tables of keel & rudder characteristics for different angles of attack, speeds, water conditions and planform size.
  • Export tables to .csv file format for use in spreadsheet programs.
  • Export 3D wings to .stl file format for virtual prototyping use in other CAD/CAE software.

3DFoil come with a built-in library of NACA 4, 5 & 6-digit airfoils, a cross sectional tool and water data. The full version can be used to read-in and analyze custom airfoils. The software exports tables to .csv files for easy inclusion in spreadsheet programs. It also exports a .stl file that can be imported into other CAD /CAE software packages and used by CNC machines.

More information about 3DFoil can be found at:  http://www.3dfoil.com

Request More Information About 3DFoil:
Please use the form to request more information about 3DFoil. Please describe your project & Dr. Hanley or our technical staff will contact you shortly with more information.

Name
(Required)
E-mail (Required)
Title
Organization
Street address
Address (cont.)
City
State/Province
Zip/Postal code
Country
Phone

Please enter your questions below. Thank you.

About Dr. Hanley
Dr. Patrick E. Hanley, is the owner and founder of Hanley Innovations, a small business specializing in the development of aerodynamics and fluid dynamics simulation software for education and industry. Dr. Hanley earned his B.S. degree (summa cum laude) in aerospace engineering from Polytechnic Institute of New York and his S.M. and Ph.D. degrees from the department of Aeronautics and Astronautics of Massachusetts Institute of Technology (MIT). He also completed a minor in the area of management of innovation and technology at MIT's Sloan School of Management.

After graduating from MIT, Dr. Hanley joined the Mechanical Engineering faculty at the University of Connecticut where he formulated and taught courses in aerodynamics, compressible fluids, introductory fluid mechanics and heat transfer. As a faculty member, he won the highly competitive National Science Foundation Research Initiation Award, the NASA-ASEE Summer Faculty Fellowship and three consecutive research awards from NASA Lewis Research center to study compressible viscous flows in turbomachinery using pseudospectral methods. This research led to the successful education of four (4) Ph.D students and four (4) Masters degree students. In addition Dr. Hanley can be credited with a number of publications including the pioneering work in multi-domain pseudospectral methods for compressible viscous flows entitled "A Strategy for the Efficient Simulation of Viscous Compressible Flows using a Multi-domain Pseudospectral Method" which can be found in Journal of Computational Physics, Vol 108, No. 1, pp. 153-158, September 1993.

As owner and chief software author of Hanley Innovations, Dr. Hanley has written a number of software packages including AirfoilBrowser, Airfoil Organizer, Science Graphs, VisualFoil, ModelFoil, Aerodynamics in Plain English, Center of Gravity Calculator, WingAnalysis, SmockSoft, PerpeturalPaper amongst other titles.

[ HOME | AIRFOILS | WINGS | GRAPHING | eBOOKS | ORDER]