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Wing design for blended-wing-body aircraft

Blended-Wing-Body (BWB) aircraft is a new design pitched as the future of air transport. However, due to the nature of the design that is relatively new, more research has to be made to exploit its advantages. This article studies an initial scaled blended wing body and the effect of different lift...

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Main Authors: Mat Yazik, Muhamad Hasfanizam, Hameed Sultan, Mohamed Thariq, Ariffin, Ahmad Hamdan
Format: Conference or Workshop Item
Language:English
Published: Centre for Advanced Research on Energy, Faculty of Mechanical Engineering, Universiti Teknikal Malaysia Melaka 2017
Online Access:http://psasir.upm.edu.my/id/eprint/67119/1/MERD17-2-2.pdf
http://psasir.upm.edu.my/id/eprint/67119/
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spelling my.upm.eprints.671192019-03-08T06:23:33Z http://psasir.upm.edu.my/id/eprint/67119/ Wing design for blended-wing-body aircraft Mat Yazik, Muhamad Hasfanizam Hameed Sultan, Mohamed Thariq Ariffin, Ahmad Hamdan Blended-Wing-Body (BWB) aircraft is a new design pitched as the future of air transport. However, due to the nature of the design that is relatively new, more research has to be made to exploit its advantages. This article studies an initial scaled blended wing body and the effect of different lift distribution on a BWB design. The initial design is adjusted via twist to obtain desired wing loading distribution. Aerodynamic optimization is performed on Selig S5010 aerofoil to further improve the aerodynamic performance of the BWB design. Centre for Advanced Research on Energy, Faculty of Mechanical Engineering, Universiti Teknikal Malaysia Melaka 2017 Conference or Workshop Item PeerReviewed text en http://psasir.upm.edu.my/id/eprint/67119/1/MERD17-2-2.pdf Mat Yazik, Muhamad Hasfanizam and Hameed Sultan, Mohamed Thariq and Ariffin, Ahmad Hamdan (2017) Wing design for blended-wing-body aircraft. In: 4th Mechanical Engineering Research Day 2017 (MERD'17), 30 Mar. 2017, UTeM Library, Melaka. (pp. 142-143).
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 Blended-Wing-Body (BWB) aircraft is a new design pitched as the future of air transport. However, due to the nature of the design that is relatively new, more research has to be made to exploit its advantages. This article studies an initial scaled blended wing body and the effect of different lift distribution on a BWB design. The initial design is adjusted via twist to obtain desired wing loading distribution. Aerodynamic optimization is performed on Selig S5010 aerofoil to further improve the aerodynamic performance of the BWB design.
format Conference or Workshop Item
author Mat Yazik, Muhamad Hasfanizam
Hameed Sultan, Mohamed Thariq
Ariffin, Ahmad Hamdan
spellingShingle Mat Yazik, Muhamad Hasfanizam
Hameed Sultan, Mohamed Thariq
Ariffin, Ahmad Hamdan
Wing design for blended-wing-body aircraft
author_facet Mat Yazik, Muhamad Hasfanizam
Hameed Sultan, Mohamed Thariq
Ariffin, Ahmad Hamdan
author_sort Mat Yazik, Muhamad Hasfanizam
title Wing design for blended-wing-body aircraft
title_short Wing design for blended-wing-body aircraft
title_full Wing design for blended-wing-body aircraft
title_fullStr Wing design for blended-wing-body aircraft
title_full_unstemmed Wing design for blended-wing-body aircraft
title_sort wing design for blended-wing-body aircraft
publisher Centre for Advanced Research on Energy, Faculty of Mechanical Engineering, Universiti Teknikal Malaysia Melaka
publishDate 2017
url http://psasir.upm.edu.my/id/eprint/67119/1/MERD17-2-2.pdf
http://psasir.upm.edu.my/id/eprint/67119/
_version_ 1643838810736295936
score 13.188404

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