SimScale simulation projects by alfiosky4 | Page 1

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Apollo Command Module  in - transonic speed reentry interface - compressible analysis.

First test on a rocket ogive to be printed in 3D.

Some compressible and incompressible simulations on Dassault Mirage 2000 - Delta Wing - jet.
- High AoA flight: 15 degrees Angle of attack at 195 Kts (Landing configuration) flow visualization.
- Supersonic Flight: mach 1.5 at 32.000 ft. Bowshock visualization.
- Inlet flow visualization

LERX stands for Leading-Edge Root extension. Its primarily purpose Is to improve airflow and handling at low Speed and High angle of Attack. This special surface generates a controlled vortex to energize airflow and retard stall.

A dynamic analysis project to demonstrate the positive influence of adding a covering case on an iPhone 6.

Observing differences on flow around a car with open and closed windows.

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