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Skywalker x8Aerodynamic Analysis (Copy)
352 1
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2 Geometries 1 Mesh 0 Simulation setups 0 Results
About this project
An aerodynamic analysis of the SKywalker x8 in which we calculate the drag coefficiency in order to enhance the fuselage design
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by Ali_ArafatAli_Arafat
Project History
george_popescu created this project
mjelemalaba copied this project