EXPERIMENTAL INVESTIGATION OF AEROELASTIC DEFORMATIONS OF A FLAPPING WING WITH IMAGE PROCESSING TECHNIQUE
In recent decades, flapping-wing micro aerial vehicles (FWMAVs) have shown an increased interest for flight at low Reynolds numbers. Major components of a flapping wing system are...
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| Format: | Article |
| Language: | fas |
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Sharif University of Technology
2019-05-01
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| Series: | مهندسی مکانیک شریف |
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| Online Access: | https://sjme.journals.sharif.edu/article_20843_7443a13cdfb69fadaad01c61ecd21f53.pdf |