Approximate function for unsteady aerodynamic kernel function of aeroelastic lifting surfaces

Prediction of unsteady aerodynamic loads is still the most challenging tasks in flutter aeroelastic analysis. Generally, the numerical estimation of steady and unsteady aerodynamics of thin lifting surface is conducted based on an integral equation relating aerodynamic pressure and normal wash ve...

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Bibliographic Details
Main Authors: Sulaeman, Erwin, Ahmed, Layeeq
Format: Article
Language:English
Published: IIUM Press 2014
Subjects:
Online Access:http://irep.iium.edu.my/41696/1/504-2058-4-PB.pdf
http://irep.iium.edu.my/41696/
http://journals.iium.edu.my/ejournal/index.php/iiumej/index
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