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...

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Main Authors: Abdul Hamid, Mohd Faisal, Gires, Ezanee, Mohd Harithuddin, Ahmad Salahuddin, Abu Talib, Abd Rahim, Mohd Rafie, Azmin Shakrine, Romli, Fairuz Izzuddin, Harmin, Mohammad Yazdi
Format: Article
Language:English
Published: Institute of Physics Publishing 2017
Online Access:http://psasir.upm.edu.my/id/eprint/61133/1/Coanda%20configured%20aircraft%20a%20preliminary%20analytical%20assessment.pdf
http://psasir.upm.edu.my/id/eprint/61133/
http://iopscience.iop.org/article/10.1088/1757-899X/270/1/012004/pdf
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spelling my.upm.eprints.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
institution Universiti Putra Malaysia
building UPM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Putra Malaysia
content_source UPM Institutional Repository
url_provider http://psasir.upm.edu.my/
language English
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.
format Article
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
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
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
title Coanda configured aircraft: a preliminary analytical assessment
title_short 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_sort coanda configured aircraft: a preliminary analytical assessment
publisher Institute of Physics Publishing
publishDate 2017
url http://psasir.upm.edu.my/id/eprint/61133/1/Coanda%20configured%20aircraft%20a%20preliminary%20analytical%20assessment.pdf
http://psasir.upm.edu.my/id/eprint/61133/
http://iopscience.iop.org/article/10.1088/1757-899X/270/1/012004/pdf
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score 13.209306