| Display title | Physics:Drag polar |
| Default sort key | Drag polar |
| Page length (in bytes) | 13,644 |
| Namespace ID | 3020 |
| Namespace | Physics |
| Page ID | 642201 |
| 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 |
| HandWiki item ID | None |
| Edit | Allow all users (infinite) |
| Move | Allow all users (infinite) |
| Page creator | imported>Steve Marsio |
| Date of page creation | 02:20, 24 September 2021 |
| Latest editor | imported>Steve Marsio |
| Date of latest edit | 02:20, 24 September 2021 |
| 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. | User:RMCD bot/subject notice
The drag polar or drag curve is the relationship between the lift on an aircraft and its drag, expressed in terms of the dependence of the drag coefficient on the lift coefficient. It may be described by an equation or displayed in a diagram called a polar plot. |
