Investigation of aerodynamic parameters of a hybrid airship

The aerodynamic parameters of a preliminary winged-hull airship design are investigated. The research methodology involved the use of numerical simulation and wind tunnel testing. The aerodynamic parameters of the design are first computed using a commercial CFD code. The force and moment coefficien...

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Main Authors: Andan, Amelda Dianne, Asrar, Waqar, Omar, Ashraf Ali
Format: Article
Language:English
Published: American Institute of Aeronautical and Astronautic 2012
Subjects:
Online Access:http://irep.iium.edu.my/26573/
http://irep.iium.edu.my/26573/
http://irep.iium.edu.my/26573/
http://irep.iium.edu.my/26573/1/Investigation_of_Aerodynamic.pdf
id iium-26573
recordtype eprints
spelling iium-265732012-11-12T03:32:10Z http://irep.iium.edu.my/26573/ Investigation of aerodynamic parameters of a hybrid airship Andan, Amelda Dianne Asrar, Waqar Omar, Ashraf Ali TL500 Aeronautics The aerodynamic parameters of a preliminary winged-hull airship design are investigated. The research methodology involved the use of numerical simulation and wind tunnel testing. The aerodynamic parameters of the design are first computed using a commercial CFD code. The force and moment coefficients are then measured on a scaled model in the IIUM low speed wind tunnel. The experimental results generally agree with the CFD predicted data. Addition of a wing to conventional airship increases the lift substantially with a reasonable increase in drag. The longitudinal and directional stabilities were found to be statically stable, however, both the conventional airship and the hybrid airship were found to have poor rolling stability. CFD simulations show that modifications to the wing placement and its dihedral have strong positive effect on the rolling stability. American Institute of Aeronautical and Astronautic 2012-03-01 Article PeerReviewed application/pdf en http://irep.iium.edu.my/26573/1/Investigation_of_Aerodynamic.pdf Andan, Amelda Dianne and Asrar, Waqar and Omar, Ashraf Ali (2012) Investigation of aerodynamic parameters of a hybrid airship. Journal of Aircraft, 49 (2). pp. 658-661. ISSN 0021-8669 http://arc.aiaa.org/doi/abs/10.2514/1.C031491 10.2514/1.C031491
repository_type Digital Repository
institution_category Local University
institution International Islamic University Malaysia
building IIUM Repository
collection Online Access
language English
topic TL500 Aeronautics
spellingShingle TL500 Aeronautics
Andan, Amelda Dianne
Asrar, Waqar
Omar, Ashraf Ali
Investigation of aerodynamic parameters of a hybrid airship
description The aerodynamic parameters of a preliminary winged-hull airship design are investigated. The research methodology involved the use of numerical simulation and wind tunnel testing. The aerodynamic parameters of the design are first computed using a commercial CFD code. The force and moment coefficients are then measured on a scaled model in the IIUM low speed wind tunnel. The experimental results generally agree with the CFD predicted data. Addition of a wing to conventional airship increases the lift substantially with a reasonable increase in drag. The longitudinal and directional stabilities were found to be statically stable, however, both the conventional airship and the hybrid airship were found to have poor rolling stability. CFD simulations show that modifications to the wing placement and its dihedral have strong positive effect on the rolling stability.
format Article
author Andan, Amelda Dianne
Asrar, Waqar
Omar, Ashraf Ali
author_facet Andan, Amelda Dianne
Asrar, Waqar
Omar, Ashraf Ali
author_sort Andan, Amelda Dianne
title Investigation of aerodynamic parameters of a hybrid airship
title_short Investigation of aerodynamic parameters of a hybrid airship
title_full Investigation of aerodynamic parameters of a hybrid airship
title_fullStr Investigation of aerodynamic parameters of a hybrid airship
title_full_unstemmed Investigation of aerodynamic parameters of a hybrid airship
title_sort investigation of aerodynamic parameters of a hybrid airship
publisher American Institute of Aeronautical and Astronautic
publishDate 2012
url http://irep.iium.edu.my/26573/
http://irep.iium.edu.my/26573/
http://irep.iium.edu.my/26573/
http://irep.iium.edu.my/26573/1/Investigation_of_Aerodynamic.pdf
first_indexed 2023-09-18T20:39:33Z
last_indexed 2023-09-18T20:39:33Z
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