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Blended Wing Body Aircraft flow simulation
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Statistics
1 Geometry
1 Mesh
1 Simulation setup
2 Results
1 Geometry 1 Mesh 1 Simulation setup 2 ResultsAbout this project
This project aims to find out the effect of the blended wing on the performances of the aircraft and to optimize the design of the blended wing. For this project compressible type of simulation has been chosen because the aircraft with blended wing body moves at high velocity
