Shock waves
Fluid mechanics-One-dimensionnal compressible flow
Article REF: BE8165 V1
Shock waves
Fluid mechanics-One-dimensionnal compressible flow

Author : André LALLEMAND

Publication date: September 10, 2014, Review date: January 4, 2020 | Lire en français

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6. Shock waves

A shockwave is a very thin zone of flow, less than 1 mm thick, which marks the transition from supersonic velocity upstream to subsonic velocity downstream. In the same space, pressure rises sharply. As a result, the fluid particles passing through the shockwave undergo an extremely high deceleration rate of up to 10 9 to 10 10 m /s 2 , or around one billion g. It's this violent impact, producing a real shock on the particles, which is the origin of the name given to this transition zone.

There are straight (or flat) shockwaves and oblique shockwaves.

6.1 Straight shock waves

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