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Hovercraft Mk. 1
611
5
Statistics
21Â Geometries
27Â Meshes
15Â Simulation setups
39Â Results
21Â Geometries 27Â Meshes 15Â Simulation setups 39Â ResultsAbout this project
Goal: Calculate drag coefficient for hovercraft. Simulation type: CFD Wind Tunnel analysis. A 3D model of a physical hovercraft is uploaded and tested in a virtual wind tunnel to calculate its drag coefficient. This is for a research paper regarding hovercraft thrust systems. My initial estimate is a drag coefficient of 0.5, based on typical values of hovercraft drag coefficients given in the literature.
