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Normal Shock

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Normal shock states

M1 2.000 to M2 0.577

The existing interactive shock view compares upstream, shock, and downstream states.

Hover upstream, downstream, or the shock wave to highlight the corresponding values.

Normal Shock Details

Hover over the visualization to explore shock properties

Upstream Mach number

2.000

State 1

Downstream Mach number

0.577

State 2

Pressure ratio

4.500

p2/p1

Temperature ratio

1.687

T2/T1

Density ratio

2.667

rho2/rho1

Total pressure loss

27.91%

Entropy change 0.3273 delta-s/R

Open Source and Easy to Use Elsewhere

This tool is open source and the underlying logic is fully transparent. You can inspect the code, understand the calculations, and contribute improvements. If you want to use the tool in your own website, course page, or learning platform, you can also embed it directly and start from a ready-made iframe setup for this exact tool.

Open source: review the implementation and see how the results are produced.

Embeddable: preview this tool, copy the iframe, and use it in your own site or LMS.