| Display title | Engineering:Thickness-to-chord ratio |
| Default sort key | Thickness-to-chord ratio |
| Page length (in bytes) | 6,892 |
| Namespace ID | 3034 |
| Namespace | Engineering |
| Page ID | 603901 |
| Page content language | en - English |
| Page content model | wikitext |
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| Counted as a content page | Yes |
| Page image |  |
| HandWiki item ID | None |
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| Page creator | imported>QCDvac |
| Date of page creation | 16:44, 9 July 2022 |
| Latest editor | imported>QCDvac |
| Date of latest edit | 16:44, 9 July 2022 |
| Total number of edits | 1 |
| Recent number of edits (within past 90 days) | 0 |
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Description | Content |
Article description: (description)
This attribute controls the content of the description and og:description elements. | In aeronautics, the thickness-to-chord ratio, sometimes simply chord ratio or thickness ratio, compares the maximum vertical thickness of a wing to its chord. It is a key measure of the performance of a wing planform when it is operating at transonic speeds.
At speeds approaching the speed of sound, |
