Abstract
The possibility of incorporating endplates to a biplane was explored. Induced drag was reduced and span efficiency was increased. This effect can help increase the lift to drag ratio of biplane configuration lifting system.
| Original language | English |
|---|---|
| Pages (from-to) | 398-400 |
| Number of pages | 3 |
| Journal | Journal of Aircraft |
| Volume | 38 |
| Issue number | 2 |
| DOIs | |
| Publication status | Published - 2001 |
| Externally published | Yes |
ASJC Scopus subject areas
- Aerospace Engineering