Lift Distributions On Low Aspect Ratio Wings At Low Reynolds Numbers
The aerodynamic performance of low aspect ratio wings at low Reynolds numbers applicable to micro air vehicle design was studied in this thesis. There is an overall lack of data for this low Reynolds number range, particularly concerning details of local flow behavior along the span. Experiments wer...
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Others |
| Published: |
Digital WPI
2004
|
| Subjects: | |
| Online Access: | https://digitalcommons.wpi.edu/etd-theses/371 https://digitalcommons.wpi.edu/cgi/viewcontent.cgi?article=1370&context=etd-theses |