Stagnation pressure
Builds on Isentropic flowMach numberBernoulli's principleShock wave
Definition
Consider a fluid particle with static pressure , density and speed . Its stagnation pressure is the pressure it would have after being brought to rest by an isentropic process, that is, adiabatically and reversibly.
- For an incompressible fluid, .
- For an ideal gas with constant ratio of specific heats , at Mach number ,
Remarks
Example: air at moving at with has . For small the binomial expansion gives , which recovers formula 1 as . In steady inviscid flow without heat exchange is constant along streamlines, which is a form of Bernoulli's principle. Non-example: the static pressure is not a stagnation pressure, because it is measured moving with the fluid and does not include the kinetic energy. Across a shock wave the stagnation pressure drops, since the process is not reversible.
Reading path
To understand this page from the ground up, read these 10 pages in order. The foundations come first.
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- no evidence level
- Euler equations concept
- Inviscid flow concept
- Isentropic flow concept
- Mach number concept
- Shock wave concept
- Streamlines, streaklines and pathlines concept
- Velocity potential concept
- Vorticity concept
- Bernoulli's principle statement
- Stagnation pressure definition
Further reading
About this page
| Tag | 3AFWE792TA |
|---|---|
| URI | m2://3AFWE792TA |
| Kind | definition |
| Writing | W0 stub |
| MSC | 76N15, 76G25 |
| Defines | Stagnation pressure |
| Uses | Isentropic flow, Mach number, Bernoulli's principle, Shock wave |
| Changed | 3 November 2026 |
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