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: | Erwin Sulaeman, Layeeq Ahmed |
---|---|
Format: | Article |
Language: | English |
Published: |
IIUM Press, International Islamic University Malaysia
2014-05-01
|
Series: | International Islamic University Malaysia Engineering Journal |
Online Access: | http://journals.iium.edu.my/ejournal/index.php/iiumej/article/view/504 |
Similar Items
-
Unsteady Lifting Line Theory Using the Wagner Function for the Aerodynamic and Aeroelastic Modeling of 3D Wings
by: Johan Boutet, et al.
Published: (2018-09-01) -
Aeroelastic Instabilities due to Unsteady Aerodynamics
by: Besem, Fanny Maud
Published: (2015) -
Unsteady Aerodynamic and Aeroelastic Analysis of Flapping Flight
by: Gopalalkrishnan, Pradeep
Published: (2014) -
Unsteady aerodynamics for aeroelastic applications using the impulse response method
by: Guendel, Randal Edmund, 1975-
Published: (2005) -
Improved unsteady aerodynamic influence coefficients for dynamic aeroelastic response
by: Murphy, Quinn
Published: (2013)