Experimental and numerical study on the aerodynamics and stability characteristics of a canard aircraft

Modern day fighter aircrafts are mostly canard configured because of its advantages over conventional configuration. The primary objective of this work is to investigate the low speed aerodynamic and stability characteristics of a canard configured aircraft. Using CFD -ANSYS Fluent package, numeric...

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Main Authors: Syed Mohamed Ali, Jaffar, M. Saleh, Mubin
Format: Article
Language:English
English
Published: Penerbit Akademia Baru 2019
Subjects:
Online Access:http://irep.iium.edu.my/68505/
http://irep.iium.edu.my/68505/1/68505_Experimental%20and%20numerical%20study.pdf
http://irep.iium.edu.my/68505/2/68505_Experimental%20and%20numerical%20study_SCOPUS.pdf
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author Syed Mohamed Ali, Jaffar
M. Saleh, Mubin
author_facet Syed Mohamed Ali, Jaffar
M. Saleh, Mubin
author_sort Syed Mohamed Ali, Jaffar
building IIUM Repository
collection Online Access
description Modern day fighter aircrafts are mostly canard configured because of its advantages over conventional configuration. The primary objective of this work is to investigate the low speed aerodynamic and stability characteristics of a canard configured aircraft. Using CFD -ANSYS Fluent package, numerical flow simulations were carried out for a typical canard configuration such as Burt Rutan’s VariEze, a composite homebuilt canard aircraft. To validate the numerical results, wind tunnel testing of a scaled model was carried out. Finally the effect of horizontal location of canard on the aerodynamics and stability characteristics was studied.
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institution International Islamic University Malaysia
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language English
English
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spelling iium-685052019-05-29T02:09:11Z http://irep.iium.edu.my/68505/ Experimental and numerical study on the aerodynamics and stability characteristics of a canard aircraft Syed Mohamed Ali, Jaffar M. Saleh, Mubin TL Motor vehicles. Aeronautics. Astronautics Modern day fighter aircrafts are mostly canard configured because of its advantages over conventional configuration. The primary objective of this work is to investigate the low speed aerodynamic and stability characteristics of a canard configured aircraft. Using CFD -ANSYS Fluent package, numerical flow simulations were carried out for a typical canard configuration such as Burt Rutan’s VariEze, a composite homebuilt canard aircraft. To validate the numerical results, wind tunnel testing of a scaled model was carried out. Finally the effect of horizontal location of canard on the aerodynamics and stability characteristics was studied. Penerbit Akademia Baru 2019-01-01 Article PeerReviewed application/pdf en http://irep.iium.edu.my/68505/1/68505_Experimental%20and%20numerical%20study.pdf application/pdf en http://irep.iium.edu.my/68505/2/68505_Experimental%20and%20numerical%20study_SCOPUS.pdf Syed Mohamed Ali, Jaffar and M. Saleh, Mubin (2019) Experimental and numerical study on the aerodynamics and stability characteristics of a canard aircraft. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 53 (2). pp. 165-174. ISSN 2289-7879 http://www.akademiabaru.com/doc/ARFMTSV53_N2_P165_174.pdf
spellingShingle TL Motor vehicles. Aeronautics. Astronautics
Syed Mohamed Ali, Jaffar
M. Saleh, Mubin
Experimental and numerical study on the aerodynamics and stability characteristics of a canard aircraft
title Experimental and numerical study on the aerodynamics and stability characteristics of a canard aircraft
title_full Experimental and numerical study on the aerodynamics and stability characteristics of a canard aircraft
title_fullStr Experimental and numerical study on the aerodynamics and stability characteristics of a canard aircraft
title_full_unstemmed Experimental and numerical study on the aerodynamics and stability characteristics of a canard aircraft
title_short Experimental and numerical study on the aerodynamics and stability characteristics of a canard aircraft
title_sort experimental and numerical study on the aerodynamics and stability characteristics of a canard aircraft
topic TL Motor vehicles. Aeronautics. Astronautics
url http://irep.iium.edu.my/68505/
http://irep.iium.edu.my/68505/
http://irep.iium.edu.my/68505/1/68505_Experimental%20and%20numerical%20study.pdf
http://irep.iium.edu.my/68505/2/68505_Experimental%20and%20numerical%20study_SCOPUS.pdf