سال انتشار: ۱۳۸۶

محل انتشار: هفتمین همایش انجمن هوافضای ایران

تعداد صفحات: ۱۰

نویسنده(ها):

Sh. Shams – Phd Candidate, Dept. of Aerospace Eng., Amirkabir Univ. of Tech., Tehran, Iran
M.H. Sadr Lahidjani – Assistant Professor, Dept. of Aerospace Eng., Amirkabir Univ. of Tech., Tehran, Iran
H. Haddadpour – Assistant Professor, Sharif Univ. of Tech., Tehran, Iran
M. Malekian – Msc Student, Dept. of Aerospace Eng., Amirkabir Univ. of Tech., Tehran, Iran

چکیده:

This paper presents a new approach in the computational aeroelasticity for deriving the equations of a two dimensional airfoil considering the nonlinear heaving and pitching stiffeners for structural modeling and the unsteady airstreams based on the Wagner integral function as aerodynamics loading. In this approach a new form of the equations can be obtained by derivation from the primary nonlinear integro-differential aeroelastic equations. The mentioned equations that are in the form of ordinary differential equations can be solved by the ordinary numeric methods such as Runge-Kutta etc. The obtained results for a test case show good agreement with those of the some other researches.