A NUMERICAL AND EXPERIMENTAL STUDY FOR AERODYNAMIC THRUST OPTIMIZATION
Flapping wings draw considerable attention due to their advantages in lift and thrust recovery in low Reynolds number fight, where they can be used as an alternative to conventional micro air vehicle (MAV) designs. The application areas of MAVs has widened with the development of new flight techniqu...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Hezarfen Aeronautics and Space Technologies Institue
2016-07-01
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| Series: | Havacılık ve Uzay Teknolojileri Dergisi |
| Subjects: | |
| Online Access: | http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/36/29 |