2438x
30x
003370
2022-05-19

A numerical simulation of the flow around a glider has been performed with different angles of attack in RWIND 2. The main goal is to simulate a flow around the wings and fuselage of a glider and to determine the drag and lift coefficient with respect to the angle of attack. The critical angle of attack, i.e. the angle of attack which produces the maximum lift coefficient, can be identified.


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Flow Around Glider | CFD Simulation

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