Numerical simulation of jet flow impinging on a shielded Hartmann resonator.

This project was awarded to Mohitsrivastav for $180 USD.

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Numerical methodology is to be used to study the effect of shield on the flow characteristics of a Hartmann resonator. The shield diameter is changed during the study to find the effect on the flow instabilities in front of the resonator inlet. The Hartmann resonator is provided with a chamfer angle of 15.

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