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Dateigröße
21,652,696 Bytes
MD5
9f72dc3a31736e28abb22821b623e0a4

Projektbeschreibung

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.