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
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
