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Hovercraft Mk. 1
219
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Statistics
16Â Geometries
19Â Meshes
10Â Simulation setups
25Â Results
16Â Geometries 19Â Meshes 10Â Simulation setups 25Â 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.
