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Testing Delta Wing Airfoil Implemented onto Modern Airbus a350 fuselage
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1 Geometry 1 Mesh 1 Simulation setup 0 Results
About this project
Analyzing velocity irregularites, pressure distribution/gradient along aircraft surface, and lift/drag coefficient within limited time set.
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by Ali_ArafatAli_Arafat
Project History
nuvahuja1 created this project