Computational aerodynamic analysis on perimeter reinforced (PR)-compliant wing
Implementing the morphing technique on a micro air vehicle (MAV) wing is a very challenging task, due to the MAV's wing size limitation and the complex morphing mechanism. As a result, understanding aerodynamic characteristics and flow configurations, subject to wing structure deformation of a...
| الحاوية / القاعدة: | Chinese Journal of Aeronautics |
|---|---|
| المؤلف الرئيسي: | |
| التنسيق: | مقال |
| اللغة: | English |
| منشور في: |
2013
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| الوصول للمادة أونلاين: | https://www.scopus.com/inward/record.uri?eid=2-s2.0-84886084661&doi=10.1016%2fj.cja.2013.09.001&partnerID=40&md5=9ead7c71dd65429c2ed1ada537834dad |