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Faculty of Engineering
Document Details
Document Type
:
Article In Journal
Document Title
:
The Finite Element Technique in the Determination of Wing Flutter Speed of Aircraft
استخدام طريقة العناصر المتناهية في تحديد سرعة الطائرة عند رفرفة الجناح
Subject
:
Aeronautical Engineering
Document Language
:
English
Abstract
:
The determination of flutter speed of aircraft is of a prime importance. This is done to ensure that the aircraft is flutter free within its flight envelope. The present method for the determination of flutter speed uses the finite element technique to calculate the mass and stiffness distribution of the whole structure of the aircraft and hence to compute the natural frequencies and the mode shapes of the complete structure. After adding the aerodynamic forces Theodorsen method is used to solve the flutter stability determinant, and1the flutter speed is determined by the point of intersection of the real and imaginary root loci. The present method is used to determine the flutter speed of a commuter airliner and the results are given.
ISSN
:
1319-1047
Journal Name
:
Engineering Sciences Journal
Volume
:
3
Issue Number
:
1
Publishing Year
:
1411 AH
1991 AD
Article Type
:
Article
Added Date
:
Saturday, January 2, 2010
Researchers
Researcher Name (Arabic)
Researcher Name (English)
Researcher Type
Dr Grade
Email
محمود نديم نحاس
Nahas, Mahmoud Nadeem
Researcher
Doctorate
Files
File Name
Type
Description
24624.pdf
pdf
The Finite Element Technique in the Determination of Wing Flutter Speed of Aircraft
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