Reconstruction of Modal Analysis for Bahwing by Solid and Shell Element

Nanda Wirawan and Mahesa Akbar (2015) Reconstruction of Modal Analysis for Bahwing by Solid and Shell Element. Proceedings International Seminar of Aerospace Science and Technology, 2015. pp. 26-33.

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Abstract

A jet transport wing plan form which commonly cited as BAH Wing (Bisplinghoff, Ashley, Halfman, 1971) has been used in various researches as one of the standards in aeroelasticity field. BAH wing in its origin, was utilized to perform modal analysis and also static (divergence) and dynamic (flutter) aeroelasticity analysis.In this paper, BAH wing modal analysis is reconstructed by solid and shell elements using MSC PATRAN/NASTRAN software. The normal modes and natural frequencies are compared with the original platform analysis by (Bisplinghoff, Ashley, & Halfman, 1971) and also the results by (MSC.Nastran Aeroelastic Analysis User’s Guide, 2002). The results of this paper will be further utilized to construct flutter analysis using solid and shell elements.

Item Type: Article
Additional Information: ISBN 978-602-71833-1-5
Uncontrolled Keywords: BAH wing, modal analysis, normal mode, natural frequency, lumped mass, shell element, solid element
Subjects: Teknologi Penerbangan dan Antariksa > Penelitian, Pengembangan, Perekayasaan, dan Pemanfaatan > Teknologi Aeronautika
Divisions: Deputi Teknologi Penerbangan Dan Antariksa > Pusat Teknologi Penerbangan
Depositing User: Dinar Indrasasi
Date Deposited: 16 Mar 2021 13:36
Last Modified: 23 Sep 2021 23:46
URI: http://repositori.lapan.go.id/id/eprint/451

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