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CFD-Rocket |
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CFD-Rocket is
a general-purpose finite element method based, unstructured grid compressible
flow solver. CFD-Rocket generates hybrid triangle and quadrilateral elements
for 2D computational domain and by sweeping the 2D mesh around the axis line
plus pre-specified number of wings and wing cross-section shape, a 3D mesh
for wings and body combinations can be easily generated within minutes. The
generated 3D meshes will consist of the hexahedral, prisms, pyramids and the
tetrahedral. All necessary information, such as boundary conditions, initial
conditions, solid wall and farfield conditions will also be written into the
generated 3D mesh file. Users can run the solver immediately
after the mesh file was generated. Contact
Email: cfdrocket@gmail.com FluSol-FEM Solver Disclaimer and Engineering Use
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Mach 1.97 flows past NACA RM-A56G16 missile at 12o angle of attack. |
30 Days License Updated Download
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Mach 1.2 flow past the elliptical rocket at 10 degrees angle of attack. |
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Mach 1.62 flows past NACA RM-10 missile at 2o angle of attack. |
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3D Conical Flow |
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