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Shockwave detection in convergent divergent nozzle

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Project mainly focuses on capturing of shockwave at the outlet of converging diverging nozzle with inlet velocity at 250ms or more . Detection of shock has been main research focus in the field of aerodynamics and numerous effects on the body generating shock . Also data can be used for the study of aeroacoustics for calculation of sound pressure level and sources of acoustics.

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Project History

  • manojs

    manojs created this project