Coanda configured aircraft: a preliminary analytical assessment
The interest in the use of flow control for enhanced aerodynamic performance has grown, particularly in the use of jets (continuous, synthetic, pulsed, etc.), compliant surface, vortex-cell, and others. It has been widely documented that these active control concepts can dramatically alter the behav...
| Main Authors: | , , , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Institute of Physics Publishing
2017
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| Online Access: | http://psasir.upm.edu.my/id/eprint/61133/ http://psasir.upm.edu.my/id/eprint/61133/1/Coanda%20configured%20aircraft%20a%20preliminary%20analytical%20assessment.pdf |
| _version_ | 1848854346962305024 |
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| author | Abdul Hamid, Mohd Faisal Gires, Ezanee Mohd Harithuddin, Ahmad Salahuddin Abu Talib, Abd Rahim Mohd Rafie, Azmin Shakrine Romli, Fairuz Izzuddin Harmin, Mohammad Yazdi |
| author_facet | Abdul Hamid, Mohd Faisal Gires, Ezanee Mohd Harithuddin, Ahmad Salahuddin Abu Talib, Abd Rahim Mohd Rafie, Azmin Shakrine Romli, Fairuz Izzuddin Harmin, Mohammad Yazdi |
| author_sort | Abdul Hamid, Mohd Faisal |
| building | UPM Institutional Repository |
| collection | Online Access |
| description | The interest in the use of flow control for enhanced aerodynamic performance has grown, particularly in the use of jets (continuous, synthetic, pulsed, etc.), compliant surface, vortex-cell, and others. It has been widely documented that these active control concepts can dramatically alter the behaviour of aerodynamic components like airfoils, wings and bodies. In this conjunction, with the present demands of low-cost and efficient flights, the use of Coandă effect as a lift enhancer has attracted a lot of interest. Tangential jets that take advantage of the Coandă effect to closely follow the contours of the body have been considered to be simple and particularly effective. For this case, a large mass of surrounding air can be entrained, hence amplifying the circulation. In an effort to optimize the aerodynamic performance of an aircraft, such effect will be critically reviewed by taking advantage of recent progress. For this purpose, in this study, the design of a Coandă-configured aircraft wing will be mathematically idealized and modelled as a two-dimensional flow problem. |
| first_indexed | 2025-11-15T11:08:25Z |
| format | Article |
| id | upm-61133 |
| institution | Universiti Putra Malaysia |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-15T11:08:25Z |
| publishDate | 2017 |
| publisher | Institute of Physics Publishing |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | upm-611332018-09-14T07:39:18Z http://psasir.upm.edu.my/id/eprint/61133/ Coanda configured aircraft: a preliminary analytical assessment Abdul Hamid, Mohd Faisal Gires, Ezanee Mohd Harithuddin, Ahmad Salahuddin Abu Talib, Abd Rahim Mohd Rafie, Azmin Shakrine Romli, Fairuz Izzuddin Harmin, Mohammad Yazdi The interest in the use of flow control for enhanced aerodynamic performance has grown, particularly in the use of jets (continuous, synthetic, pulsed, etc.), compliant surface, vortex-cell, and others. It has been widely documented that these active control concepts can dramatically alter the behaviour of aerodynamic components like airfoils, wings and bodies. In this conjunction, with the present demands of low-cost and efficient flights, the use of Coandă effect as a lift enhancer has attracted a lot of interest. Tangential jets that take advantage of the Coandă effect to closely follow the contours of the body have been considered to be simple and particularly effective. For this case, a large mass of surrounding air can be entrained, hence amplifying the circulation. In an effort to optimize the aerodynamic performance of an aircraft, such effect will be critically reviewed by taking advantage of recent progress. For this purpose, in this study, the design of a Coandă-configured aircraft wing will be mathematically idealized and modelled as a two-dimensional flow problem. Institute of Physics Publishing 2017 Article PeerReviewed text en http://psasir.upm.edu.my/id/eprint/61133/1/Coanda%20configured%20aircraft%20a%20preliminary%20analytical%20assessment.pdf Abdul Hamid, Mohd Faisal and Gires, Ezanee and Mohd Harithuddin, Ahmad Salahuddin and Abu Talib, Abd Rahim and Mohd Rafie, Azmin Shakrine and Romli, Fairuz Izzuddin and Harmin, Mohammad Yazdi (2017) Coanda configured aircraft: a preliminary analytical assessment. IOP Conference Series: Materials Science and Engineering, 270. art. no. 012004. pp. 1-5. ISSN 1757-8981; ESSN: 1757-899X http://iopscience.iop.org/article/10.1088/1757-899X/270/1/012004/pdf 10.1088/1757-899X/270/1/012004 |
| spellingShingle | Abdul Hamid, Mohd Faisal Gires, Ezanee Mohd Harithuddin, Ahmad Salahuddin Abu Talib, Abd Rahim Mohd Rafie, Azmin Shakrine Romli, Fairuz Izzuddin Harmin, Mohammad Yazdi Coanda configured aircraft: a preliminary analytical assessment |
| title | Coanda configured aircraft: a preliminary analytical assessment |
| title_full | Coanda configured aircraft: a preliminary analytical assessment |
| title_fullStr | Coanda configured aircraft: a preliminary analytical assessment |
| title_full_unstemmed | Coanda configured aircraft: a preliminary analytical assessment |
| title_short | Coanda configured aircraft: a preliminary analytical assessment |
| title_sort | coanda configured aircraft: a preliminary analytical assessment |
| url | http://psasir.upm.edu.my/id/eprint/61133/ http://psasir.upm.edu.my/id/eprint/61133/ http://psasir.upm.edu.my/id/eprint/61133/ http://psasir.upm.edu.my/id/eprint/61133/1/Coanda%20configured%20aircraft%20a%20preliminary%20analytical%20assessment.pdf |