This project concerns the simulation of unclassified, publishable academic generic models of high-speed flow past rolling missiles._x000D_The objective of this project is to develop a methodology to correlate unsteady aerodynamic coefficients generated using Computational Fluid Dynamics (CFD) code with the steady aerodynamic coefficient predicted using engineering tools such as missile datcom. | Contrat gouvernemental · CanPursue
This project concerns the simulation of unclassified, publishable academic generic models of high-speed flow past rolling missiles._x000D_The objective of this project is to develop a methodology to correlate unsteady aerodynamic coefficients generated using Computational Fluid Dynamics (CFD) code with the steady aerodynamic coefficient predicted using engineering tools such as missile datcom.