Alternate approximate function for kernel function of oscillating lifting surfaces

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Alternate approximate function for kernel function of oscillating lifting surfaces

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 wash velocity...

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Bibliographic Details
Main Authors:	Sulaeman, Erwin, Layeeq, Ahmed
Format:	Proceeding Paper
Language:	English English
Published:	2013
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/34456/ http://irep.iium.edu.my/34456/1/Paper_30176_-_Camera_ready.pdf http://irep.iium.edu.my/34456/4/programbookicmaae13.pdf

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