Title of article
Modeling, simulation and analysis of a multi degree of freedom aircraft wing model
Author/Authors
Bi, Xueguang Stanley Security Solutions - Inc., Shenzhen, Guangdong , China , Liu, Yucheng Department of Mechanical Engineering - University of Louisiana - Lafayette, LA, USA
Pages
42
From page
21
To page
62
Abstract
conditions are considered in establishing such methods. The accuracy of the presented methods is verified by comparing the estimated aerodynamic forces with the actual values. A good agreement is achieved through the comparisons and it is verified that the present methods can be used to correctly identify the aerodynamic forces acting on the aircraft wing models.
Keywords
Freedom system , Force Determination Methods , Aircraft wing model
Journal title
نظريه تقريب و كاربردهاي آن
Serial Year
2011
Record number
2492852
Link To Document