Transonic flow
Builds on Compressible flowMach numberSpeed of soundTricomi equationShock wave
Definition
Consider a steady compressible flow past a body, with local Mach number , where is the local speed of sound. The flow is transonic if the set where and the set where are both nonempty. The surface that separates them is the sonic surface, or sonic line in a plane flow. The critical Mach number of the body is the free stream Mach number at which is first reached somewhere on the body.
Remarks
Example: a typical airfoil at free stream Mach number has a supersonic pocket above its upper surface, closed downstream by a shock wave. The flow elsewhere is subsonic, so the flow is transonic. Non-example: the same airfoil at free stream Mach number has everywhere, so the flow is subsonic. In engineering usage the transonic range is roughly . For steady irrotational flow, the potential equation is elliptic where and hyperbolic where . So a transonic flow solves a PDE of mixed type, a nonlinear relative of the Tricomi equation.
Reading path
To understand this page from the ground up, read these 6 pages in order. The foundations come first.
Show the path as a graph
- no evidence level
- Compressible flow concept
- Mach number concept
- Shock wave concept
- Speed of sound concept
- Tricomi equation concept
- Transonic flow definition
Further reading
About this page
| Tag | DDCNQDTGQW |
|---|---|
| URI | m2://DDCNQDTGQW |
| Kind | definition |
| Writing | W0 stub |
| MSC | 76H05, 35M10 |
| Defines | Transonic flow |
| Uses | Compressible flow, Mach number, Speed of sound, Tricomi equation, Shock wave |
| Changed | 3 November 2026 |
Markdown · JSON · Edit on GitHub
What this page needs for W1
- an inventory row: the row of the inventory that the node accounts for (0 of 1)
- a source with a locator (0 of 1)
The writing levels say how complete the text of a page is. They do not measure its truth.
What links here
No page links to this page yet.