1D Flows: Mach Number in a Nozzle

In course

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Description

This lecture covers the conservation of mass, energy, and momentum in 1D flows, focusing on the effects of section variation and the transition from subsonic to supersonic regimes in a nozzle. The instructor explains the isentropic flow and the relationships between Mach number and flow area.

Instructor

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Official source

https://mediaspace.epfl.ch/media/0_q3v4mkh0

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