CFD-Rocket	Visitor Counter 11639
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 Notice	Mach 1.97 flows past NACA RM-A56G16 missile at 12o angle of attack.	Samples Brochure 30 Days License Updated Download The unsteady field equation CFD with Chemical reactions
	Mach 1.2 flow past the elliptical rocket at 10 degrees angle of attack.
	Mach 1.62 flows past NACA RM-10 missile at 2o angle of attack.
	Mach 7.4 flow past a 75^o swept ellipse cone at 15^o angle of attack. 3D Conical Flow