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...
Main Authors: | , |
---|---|
Format: | Article |
Language: | English |
Published: |
IIUM Press
2014
|
Subjects: | |
Online Access: | http://irep.iium.edu.my/41696/ http://irep.iium.edu.my/41696/ http://irep.iium.edu.my/41696/1/504-2058-4-PB.pdf |