Application #36. Dynamic Overset Grid Demonstration Using A Simple Rotor/Fuselage Model
Contributed by Dave O’Brien and Marilyn Smith, Georgia Tech
Simple proof of concept for dynamic overset grid capability within FUN3D. The movie shows pressure coefficient variation over a half revolution in 6 degree intervals. The rotor blade grid moves within a stationary fuselage grid. Overset capabilities are achieved using the DiRTlib and SUGGAR programs.
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NASA Official: David P. Lockard
Contact: FUN3D-support@lists.nasa.gov
Page Last Modified: 2024-04-25 10:30:27 -0400
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