SimScale simulation projects by Get_Barried | Page 1

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NOTE (11/1/2020): With removal of rhoCentralFoam from Simscale. This project is now unable to continue is obsolete.

This project aims to validate various diamond aerofoils at varying degrees and mach numbers against a Theta-Beta-Mach Oblique Shock Table.

To find the drag for a Hyperloop pod, 1.8m dia, in a 2.6m tube. With the 2:1 tube/pod area ratio, the airflow in the narrow throat is faster or more compressed. The vacuum, about 100Pa (1/1000 atm), will reduce the drag forces. Would like speeds up to 250 m/s, but it's challenging with maybe transonic flow in the throat.

https://www.simscale.com/forum/t/errors-in-low-pressure-compressible-flow-hyperloop/81813

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