Description: James formats based on the CFD program to calculate the flow field and the NACA0012 airfoil lift drag coefficient. Fluent grid provided by the Gmbit generated, calculated results can Tecplot Views
- [Galerkin--Euler] - procedure is used for writing, no such s
- [nso] - right 2D viscous incompressible Navier-S
- [twophase] - Stream function method based on particle
- [2Dfd] - 2D finite difference method, without bou
- [compiler] - This is using java prepared statements f
- [pablo] - Can generate a standard airfoil coordina
- [Muscl_Euler_Two_dimensions] - Muscl Euler Two dimensions
- [pscnc] - PIC-SERVO CNC: 3-Axis Milling Machine Co
- [CFDroe] - CFD, based on the finite volume method,
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