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Shockwave detection in convergent divergent nozzle
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1 Geometry
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1 Geometry 1 Mesh 0 Simulation setups 0 ResultsAbout this project
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.
