Flutter analysis of supersonic wing with external stores

One of the most dangerous aeroelastic failure phenomenon is flutter. The flutter characteristic is different for each type of aircraft depends on the wing geometry and its operational region of subsonic, transonic or supersonic. Prior to performing flight flutter test, extensive numerical simulation...

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Main Authors:	Abdullah, Nur Azam, Sulaeman, Erwin
Format:	Conference or Workshop Item
Language:	English English
Published:	2013
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/34446/ http://irep.iium.edu.my/34446/ http://irep.iium.edu.my/34446/1/Paper_30160_-_Camera_ready.pdf http://irep.iium.edu.my/34446/4/programbookicmaae13.pdf

id	iium-34446
recordtype	eprints
spelling	iium-344462019-10-31T08:35:18Z http://irep.iium.edu.my/34446/ Flutter analysis of supersonic wing with external stores Abdullah, Nur Azam Sulaeman, Erwin TL500 Aeronautics One of the most dangerous aeroelastic failure phenomenon is flutter. The flutter characteristic is different for each type of aircraft depends on the wing geometry and its operational region of subsonic, transonic or supersonic. Prior to performing flight flutter test, extensive numerical simulations and Ground Vibration Test should be conducted where the structural finite element modes and the experimentation results should be matched otherwise the numerical simulation model could be rejected. In the present paper, the simulation of supersonic wing equipped with external loads of missiles on the wing had been analyzed at high supersonic region. The structural mode shapes at each generated frequency mode are also visually presented. The analysis is carried out using FEM software of MSC Nastran. The wing flutter with the external stores had been simulated at different altitudes. The result shows that the flutter velocity is sensitive to the flight altitude. For this reason, the flutter analysis is conducted also for a negative altitude. The negative altitude is obtained by considering the constant equivalent speed-Mach number rule at flutter speed boundary as a requirement in standard regulation of transport aircraft. 2013-07-04 Conference or Workshop Item PeerReviewed application/pdf en http://irep.iium.edu.my/34446/1/Paper_30160_-_Camera_ready.pdf application/pdf en http://irep.iium.edu.my/34446/4/programbookicmaae13.pdf Abdullah, Nur Azam and Sulaeman, Erwin (2013) Flutter analysis of supersonic wing with external stores. In: International Conference on Mechanical, Automotive and Aerospace Engineering (ICMAAE 2013), 2nd- 4th July 2013, Berjaya Time Square Hotel, Kuala Lumpur. (Unpublished) http://www.iium.edu.my/icmaae/2013/images/M_images/programbookicmaae13.pdf
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English English
topic	TL500 Aeronautics
spellingShingle	TL500 Aeronautics Abdullah, Nur Azam Sulaeman, Erwin Flutter analysis of supersonic wing with external stores
description	One of the most dangerous aeroelastic failure phenomenon is flutter. The flutter characteristic is different for each type of aircraft depends on the wing geometry and its operational region of subsonic, transonic or supersonic. Prior to performing flight flutter test, extensive numerical simulations and Ground Vibration Test should be conducted where the structural finite element modes and the experimentation results should be matched otherwise the numerical simulation model could be rejected. In the present paper, the simulation of supersonic wing equipped with external loads of missiles on the wing had been analyzed at high supersonic region. The structural mode shapes at each generated frequency mode are also visually presented. The analysis is carried out using FEM software of MSC Nastran. The wing flutter with the external stores had been simulated at different altitudes. The result shows that the flutter velocity is sensitive to the flight altitude. For this reason, the flutter analysis is conducted also for a negative altitude. The negative altitude is obtained by considering the constant equivalent speed-Mach number rule at flutter speed boundary as a requirement in standard regulation of transport aircraft.
format	Conference or Workshop Item
author	Abdullah, Nur Azam Sulaeman, Erwin
author_facet	Abdullah, Nur Azam Sulaeman, Erwin
author_sort	Abdullah, Nur Azam
title	Flutter analysis of supersonic wing with external stores
title_short	Flutter analysis of supersonic wing with external stores
title_full	Flutter analysis of supersonic wing with external stores
title_fullStr	Flutter analysis of supersonic wing with external stores
title_full_unstemmed	Flutter analysis of supersonic wing with external stores
title_sort	flutter analysis of supersonic wing with external stores
publishDate	2013
url	http://irep.iium.edu.my/34446/ http://irep.iium.edu.my/34446/ http://irep.iium.edu.my/34446/1/Paper_30160_-_Camera_ready.pdf http://irep.iium.edu.my/34446/4/programbookicmaae13.pdf
first_indexed	2023-09-18T20:49:38Z
last_indexed	2023-09-18T20:49:38Z
_version_	1777409907942752256

Flutter analysis of supersonic wing with external stores

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