Hovercraft Mk. 1

About 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.