SimScale simulation projects by bzalla10 | Page 1

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Simulating rocket for center of pressure and drag coefficient.

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.

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