An experimental mechanism of a tandem flapping wing for micro aerial vehicle
Micro Aerial Vehicles, otherwise known as MAVs, is defined as an aerial vehicle that has a 15cm or less wingspan with a take off wight of less than 200g. Its miniature size and manoeuvrability allows it to fly in confined space at low Reynolds number flight conditions (100 - 100,000). In this study,...
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Institute of Physics Publishing
2019
|
| Subjects: | |
| Online Access: | View Fulltext in Publisher View in Scopus |