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Airfoil Applet: Hess-Smith Panel Method

        

Airfoil Applet: Hess-Smith Panel Method

Logo for Airfoil Applet:  Hess-Smith Panel Method
Online applet calculates and displays lift, drag, and pressure coefficients for any 4-digit NACA airfoil.
Material Type: Simulation
Technical Format: Java Applet
Date Added to MERLOT: October 19, 2005
Date Modified in MERLOT: October 19, 2005
Author:
Send email to hhiguchi@syr.edu
Submitter: Edward Perry

Details

  • Editor Review avg: 5 rating
  • User Rating (not rated)
  • Comments (none)
  • Learning Exercises (none)
  • Personal Collections (none)
  • Accessibility Info (none)

About

Primary Audience: High School, College General Ed, Graduate School, Professional
Mobile Compatibility: Not specified at this time
Technical Requirements: Browser capable of supporting Java applets.
Language: English
Cost Involved: no
Source Code Available: no
Accessiblity Information Available: no
Creative Commons: unsure

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