| Display title | Engineering:Turbojet |
| Default sort key | Turbojet |
| Page length (in bytes) | 29,335 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 726809 |
| Page content language | en - English |
| Page content model | wikitext |
| Indexing by robots | Allowed |
| Number of redirects to this page | 0 |
| Counted as a content page | Yes |
| Page image |  |
| HandWiki item ID | None |
| Edit | Allow all users (infinite) |
| Move | Allow all users (infinite) |
| Page creator | imported>Steve2012 |
| Date of page creation | 19:39, 4 February 2024 |
| Latest editor | imported>Steve2012 |
| Date of latest edit | 19:39, 4 February 2024 |
| Total number of edits | 1 |
| Recent number of edits (within past 90 days) | 0 |
| Recent number of distinct authors | 0 |
Description | Content |
Article description: (description)
This attribute controls the content of the description and og:description elements. | The turbojet is an airbreathing jet engine which is typically used in aircraft. It consists of a gas turbine with a propelling nozzle. The gas turbine has an air inlet which includes inlet guide vanes, a compressor, a combustion chamber, and a turbine (that drives the compressor). The compressed air... |
