An Experimental Flow Field Study of a Bio-inspired Corrugated Wing at Low Reynolds Number
The present paper examined experimentally the glide flight flow visualization and boundary layers of a bio-inspired corrugated dragonfly wing performing a comparison with the results obtained with a flat plate, at low to moderate range of chord Reynolds numbers. The experimental work is performed in...
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| Format: | Article |
| Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2019-09-01
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| Series: | INCAS Bulletin |
| Subjects: | |
| Online Access: | http://bulletin.incas.ro/files/dwivedi__sudhir-sastry__vol_11_iss_3.pdf |
| _version_ | 1818011538429050880 |
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| author | Y. D. DWIVEDI Y. B. SUDHIR SASTRY |
| author_facet | Y. D. DWIVEDI Y. B. SUDHIR SASTRY |
| author_sort | Y. D. DWIVEDI |
| collection | DOAJ |
| description | The present paper examined experimentally the glide flight flow visualization and boundary layers of a bio-inspired corrugated dragonfly wing performing a comparison with the results obtained with a flat plate, at low to moderate range of chord Reynolds numbers. The experimental work is performed in an open-end low speed subsonic wind tunnel at different angles of attack ranging from 0 to 120 and Reynolds number 2.25×105. The boundary layer measurements were done at a fixed chord location (0.7 x/c) and three different semi span locations such as 30%, 60% and 90% of the wing’s semi span from the right side of the longitudinal axis of the wing. The flow patterns were visualized by using colored tufts, placed at different span locations. The flow reversal was observed at selected Reynolds numbers and angles of attack only. The boundary layer measurements demonstrated that there exists a clear distinction on the pressure and velocity parameters in all the three tested locations on both types of the wings. The corrugated wing showed significant delay in stall and flow separation compared with the flat plate. The visualization of flow in both wings showed that there subsists a spanwise flow moving from wing tip to root, indicating three dimensional natures of airflows. |
| first_indexed | 2024-04-14T06:08:57Z |
| format | Article |
| id | doaj.art-ef542ec99ad540a580911be7f0a65c50 |
| institution | Directory Open Access Journal |
| issn | 2066-8201 2247-4528 |
| language | English |
| last_indexed | 2024-04-14T06:08:57Z |
| publishDate | 2019-09-01 |
| publisher | National Institute for Aerospace Research “Elie Carafoli” - INCAS |
| record_format | Article |
| series | INCAS Bulletin |
| spelling | doaj.art-ef542ec99ad540a580911be7f0a65c502022-12-22T02:08:26ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282019-09-01113556510.13111/2066-8201.2019.11.3.5An Experimental Flow Field Study of a Bio-inspired Corrugated Wing at Low Reynolds NumberY. D. DWIVEDI0Y. B. SUDHIR SASTRY1Department of Aeronautical Engineering, Institute of Aeronautical Engineering, Dundigal, Hyderabad, 500043, Telangana, India, yddwivedi@gmail.comDepartment of Aeronautical Engineering, Institute of Aeronautical Engineering, Dundigal, Hyderabad, 500043, Telangana, India, sudhirsastry.yb@iare.ac.inThe present paper examined experimentally the glide flight flow visualization and boundary layers of a bio-inspired corrugated dragonfly wing performing a comparison with the results obtained with a flat plate, at low to moderate range of chord Reynolds numbers. The experimental work is performed in an open-end low speed subsonic wind tunnel at different angles of attack ranging from 0 to 120 and Reynolds number 2.25×105. The boundary layer measurements were done at a fixed chord location (0.7 x/c) and three different semi span locations such as 30%, 60% and 90% of the wing’s semi span from the right side of the longitudinal axis of the wing. The flow patterns were visualized by using colored tufts, placed at different span locations. The flow reversal was observed at selected Reynolds numbers and angles of attack only. The boundary layer measurements demonstrated that there exists a clear distinction on the pressure and velocity parameters in all the three tested locations on both types of the wings. The corrugated wing showed significant delay in stall and flow separation compared with the flat plate. The visualization of flow in both wings showed that there subsists a spanwise flow moving from wing tip to root, indicating three dimensional natures of airflows.http://bulletin.incas.ro/files/dwivedi__sudhir-sastry__vol_11_iss_3.pdfbio-inspired corrugationboundary layerflow reversalspanwise flowlow Reynolds number |
| spellingShingle | Y. D. DWIVEDI Y. B. SUDHIR SASTRY An Experimental Flow Field Study of a Bio-inspired Corrugated Wing at Low Reynolds Number INCAS Bulletin bio-inspired corrugation boundary layer flow reversal spanwise flow low Reynolds number |
| title | An Experimental Flow Field Study of a Bio-inspired Corrugated Wing at Low Reynolds Number |
| title_full | An Experimental Flow Field Study of a Bio-inspired Corrugated Wing at Low Reynolds Number |
| title_fullStr | An Experimental Flow Field Study of a Bio-inspired Corrugated Wing at Low Reynolds Number |
| title_full_unstemmed | An Experimental Flow Field Study of a Bio-inspired Corrugated Wing at Low Reynolds Number |
| title_short | An Experimental Flow Field Study of a Bio-inspired Corrugated Wing at Low Reynolds Number |
| title_sort | experimental flow field study of a bio inspired corrugated wing at low reynolds number |
| topic | bio-inspired corrugation boundary layer flow reversal spanwise flow low Reynolds number |
| url | http://bulletin.incas.ro/files/dwivedi__sudhir-sastry__vol_11_iss_3.pdf |
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