Optimization of aerodynamic efficiency for twist morphing MAV wing
Twist morphing (TM) is a practical control technique in micro air vehicle (MAV) flight. However, TM wing has a lower aerodynamic efficiency (C L/CD) compared to membrane and rigid wing. This is due to massive drag penalty created on TM wing, which had overwhelmed the successive increase in its lift...
| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Chinese Journal of Aeronautics
2014
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| Subjects: | |
| Online Access: | View Fulltext in Publisher View in Scopus |