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
Submitter: Edward Perry
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.
Cost Involved: no
Source Code Available: no
Accessiblity Information Available: no
Creative Commons: unsure