Drag analysis of an aircraft wing model and without bird feather like winglet

Drag analysis of an aircraft wing model and without bird feather like winglet

This work describes the aerodynamic characteristic for aircraft wing model with and without bird feather like winglet. The aerofoil used to construct the whole structure is NACA 653-218 Rectangular wing and this aerofoil has been used to compare the result with previous research using winglet. The...

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Main Authors: Hossain, Altab, Rahman, Mohammed Ataur, Iqbal, A.K.M. Parvez, Ariffin, Muhidin, M., Mazian
Format: Article
Language:English
Published: World Academy of Science, Engineering and Technology 2012
Subjects:
TJ Mechanical engineering and machinery
Online Access:http://irep.iium.edu.my/15588/
http://irep.iium.edu.my/15588/
http://irep.iium.edu.my/15588/1/v6-1-2.pdf
id iium-15588
recordtype eprints
spelling iium-155882012-07-17T01:53:00Z http://irep.iium.edu.my/15588/ Drag analysis of an aircraft wing model and without bird feather like winglet Hossain, Altab Rahman, Mohammed Ataur Iqbal, A.K.M. Parvez Ariffin, Muhidin M., Mazian TJ Mechanical engineering and machinery This work describes the aerodynamic characteristic for aircraft wing model with and without bird feather like winglet. The aerofoil used to construct the whole structure is NACA 653-218 Rectangular wing and this aerofoil has been used to compare the result with previous research using winglet. The model of the rectangular wing with bird feather like winglet has been fabricated using polystyrene before design using CATIA P3 V5R13 software and finally fabricated in wood. The experimental analysis for the aerodynamic characteristic for rectangular wing without winglet,wing with horizontal winglet and wing with 60 degree inclination winglet for Reynolds number 1.66×105, 2.08×105 and 2.50×105 have been carried out in open loop low speed wind tunnel at the Aerodynamics laboratory in Universiti Putra Malaysia. The experimental result shows 25-30 % reduction in drag coefficient and 10-20 % increase in lift coefficient by using bird feather like winglet for angle of attack of 8 degree. World Academy of Science, Engineering and Technology 2012 Article PeerReviewed application/pdf en http://irep.iium.edu.my/15588/1/v6-1-2.pdf Hossain, Altab and Rahman, Mohammed Ataur and Iqbal, A.K.M. Parvez and Ariffin, Muhidin and M., Mazian (2012) Drag analysis of an aircraft wing model and without bird feather like winglet. International Journal of Aerospace and Mechanical Engineering, 6 (1). pp. 8-13. ISSN 2010-3794 (O), 2010-3786 (P) http://www.waset.org/journals/ijame/v6/v6-1-2.pdf
repository_type Digital Repository
institution_category Local University
institution International Islamic University Malaysia
building IIUM Repository
collection Online Access
language English
topic TJ Mechanical engineering and machinery
spellingShingle TJ Mechanical engineering and machinery
Hossain, Altab
Rahman, Mohammed Ataur
Iqbal, A.K.M. Parvez
Ariffin, Muhidin
M., Mazian
Drag analysis of an aircraft wing model and without bird feather like winglet
description This work describes the aerodynamic characteristic for aircraft wing model with and without bird feather like winglet. The aerofoil used to construct the whole structure is NACA 653-218 Rectangular wing and this aerofoil has been used to compare the result with previous research using winglet. The model of the rectangular wing with bird feather like winglet has been fabricated using polystyrene before design using CATIA P3 V5R13 software and finally fabricated in wood. The experimental analysis for the aerodynamic characteristic for rectangular wing without winglet,wing with horizontal winglet and wing with 60 degree inclination winglet for Reynolds number 1.66×105, 2.08×105 and 2.50×105 have been carried out in open loop low speed wind tunnel at the Aerodynamics laboratory in Universiti Putra Malaysia. The experimental result shows 25-30 % reduction in drag coefficient and 10-20 % increase in lift coefficient by using bird feather like winglet for angle of attack of 8 degree.
format Article
author Hossain, Altab
Rahman, Mohammed Ataur
Iqbal, A.K.M. Parvez
Ariffin, Muhidin
M., Mazian
author_facet Hossain, Altab
Rahman, Mohammed Ataur
Iqbal, A.K.M. Parvez
Ariffin, Muhidin
M., Mazian
author_sort Hossain, Altab
title Drag analysis of an aircraft wing model and without bird feather like winglet
title_short Drag analysis of an aircraft wing model and without bird feather like winglet
title_full Drag analysis of an aircraft wing model and without bird feather like winglet
title_fullStr Drag analysis of an aircraft wing model and without bird feather like winglet
title_full_unstemmed Drag analysis of an aircraft wing model and without bird feather like winglet
title_sort drag analysis of an aircraft wing model and without bird feather like winglet
publisher World Academy of Science, Engineering and Technology
publishDate 2012
url http://irep.iium.edu.my/15588/
http://irep.iium.edu.my/15588/
http://irep.iium.edu.my/15588/1/v6-1-2.pdf
first_indexed 2023-09-18T20:24:31Z
last_indexed 2023-09-18T20:24:31Z
_version_ 1777408327694680064

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