APPROXIMATE FUNCTION FOR UNSTEADY AERODYNAMIC KERNEL FUNCTION OF AEROELASTIC LIFTING SURFACES
ABSTRACT: Prediction of unsteady aerodynamic loads is still the most challenging task in flutter aeroelastic analysis. Generally the numerical estimation of steady and unsteady aerodynamic of thin lifting surface is conducted based on an integral equation relating aerodynamic pressure and normal was...
Main Authors: | , |
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Format: | Article |
Language: | English |
Published: |
IIUM Press, International Islamic University Malaysia
2014-05-01
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Series: | International Islamic University Malaysia Engineering Journal |
Online Access: | http://journals.iium.edu.my/ejournal/index.php/iiumej/article/view/504 |