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CFD simulation of RC aircraft at different AOA. (H.B)
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1 Geometry
1 Mesh
2 Simulation setups
2 Results
1 Geometry 1 Mesh 2 Simulation setups 2 ResultsAbout this project
In this project steady state incompressible fluid flow simulation of a small RC aircraft is performed for the completion of aircraft design course on SimScale's Academy. Two simulation at different AOA relative to wing is carried out to obtain the coefficient of lift and drag. Lift and drag forces are calculated at 3 and 20 AOA, also the flow around the aircraft is also visualized for the design consideration.
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by Ali_ArafatAli_Arafat
Project History
HamzaBaig created this project