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 |
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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