Folding Wing Aircraft

This is a preliminary test of a proposed project to simulate the wing fluttering of an aircraft with folding wings. This was solved using the finite volume method for 3D, steady, compressible, viscous, laminar flow on a curvilinear grid. This image shows the pressure distribution over the wings.

Folding Wing Aircraft calculated in CFL3D (Computational Fluids Laboratory 3D), rendered in POV-Ray 3.6.1, 11/3/06



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