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檔案信息

檔案大小
16,821,666 bytes
MD5
885a77c7e3ff89fcc157abb6d386f01c

專案描述

XFLR5 includes the xfoil program for foil analysis, and several 3d analysis methods for planes : - a non-linear lifting line method for standalone wings - two vortex-lattice and a 3d panel method for the analysis of aerodynamic performance of wings and plane operating at low Reynolds numbers The latest v6 version introduces stability analysis of planes.