UPM Institutional Repository

Aeroelastic analysis for Eagle 150b aircraft wing


Mohd Rafie, Azmin Shakrine and Basri, Shahnor and Varatharajoo, Renuganth and Abang Abdul Majid, Dayang Laila and Mohamed Ariff, Azmah Hanim (2009) Aeroelastic analysis for Eagle 150b aircraft wing. International Review of Aerospace Engineering, 2 (4). pp. 185-191. ISSN 1973-7459; ESSN: 2533-2279


The aim of this paper is to predict the flutter speed of an Eagle 150B aircraft wing by performing a thorough and comprehensive aeroelasticity analysis using computational techniques. There are two types of analysis conducted in this work, namely the actual wing analysis and the wing model analysis. The flutter analysis is performed using the PK-method option in the MSC Nastran and Patran software, where by eigenvalue and eigenvector are computed to determine the stability of the combined structural and aerodynamic system. Both modeling techniques show a good agreement with the experimental technique results. The results also show that the computational technique for actual wing analysis give a better prediction of flutter condition compared to wing model analysis.

Download File

Text (Abstract)
Aeroelastic analysis for Eagle 150b aircraft wing.pdf

Download (34kB) | Preview

Additional Metadata

Item Type: Article
Divisions: Faculty of Engineering
Publisher: Praise Worthy Prize
Keywords: Computational analysis; Actual wing analysis; Wing model analysis; Eagle 150B aircraft wing and flutter
Depositing User: Nabilah Mustapa
Date Deposited: 11 Jun 2018 08:38
Last Modified: 11 Jun 2018 08:38
URI: http://psasir.upm.edu.my/id/eprint/12956
Statistic Details: View Download Statistic

Actions (login required)

View Item View Item