Flutter Speed Limits of Cantilever Rectangular and Tapered Plates
The aerodynamic and elastic forces may cause an oscillation of the structure such as the high frequency of the airfoil surfaces and the dynamic instability occurring in an aircraft in flight and failure may occur at a speed called flutter speed. In this work, analytical and numerical investigations...
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Al-Khwarizmi College of Engineering – University of Baghdad
2007
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oai:doaj.org-article:fb501cf93cee4204b9d1680dbaa762652021-12-02T05:01:20ZFlutter Speed Limits of Cantilever Rectangular and Tapered Plates1818-1171https://doaj.org/article/fb501cf93cee4204b9d1680dbaa762652007-01-01T00:00:00Zhttp://www.iasj.net/iasj?func=fulltext&aId=2361https://doaj.org/toc/1818-1171The aerodynamic and elastic forces may cause an oscillation of the structure such as the high frequency of the airfoil surfaces and the dynamic instability occurring in an aircraft in flight and failure may occur at a speed called flutter speed. In this work, analytical and numerical investigations of flutter limits of thin plates have been carried out. The flutter speed of rectangular plates were obtained and compared with some published results. Different design parameters were investigated such as aspect ratio, thickness and their effects on flutter velocity. It was found that the structural mode shape plays an important role in the determination of the flutter speed and the coupling between the bending and torsional mode is the main cause of flutter.Kusay H. JabirAl-Khwarizmi College of Engineering – University of BaghdadarticleFlutterSpeedPlatesChemical engineeringTP155-156Engineering (General). Civil engineering (General)TA1-2040ENAl-Khawarizmi Engineering Journal, Vol 3, Iss 3, Pp 53-65 (2007) |
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Flutter Speed Plates Chemical engineering TP155-156 Engineering (General). Civil engineering (General) TA1-2040 |
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Flutter Speed Plates Chemical engineering TP155-156 Engineering (General). Civil engineering (General) TA1-2040 Kusay H. Jabir Flutter Speed Limits of Cantilever Rectangular and Tapered Plates |
description |
The aerodynamic and elastic forces may cause an oscillation of the structure such as the high frequency of the airfoil surfaces and the dynamic instability occurring in an aircraft in flight and failure may occur at a speed called flutter speed. In this work, analytical and numerical investigations of flutter limits of thin plates have been carried out. The flutter speed of rectangular plates were obtained and compared with some published results. Different design parameters were investigated such as aspect ratio, thickness and their effects on flutter velocity. It was found that the structural mode shape plays an important role in the determination of the flutter speed and the coupling between the bending and torsional mode is the main cause of flutter. |
format |
article |
author |
Kusay H. Jabir |
author_facet |
Kusay H. Jabir |
author_sort |
Kusay H. Jabir |
title |
Flutter Speed Limits of Cantilever Rectangular and Tapered Plates |
title_short |
Flutter Speed Limits of Cantilever Rectangular and Tapered Plates |
title_full |
Flutter Speed Limits of Cantilever Rectangular and Tapered Plates |
title_fullStr |
Flutter Speed Limits of Cantilever Rectangular and Tapered Plates |
title_full_unstemmed |
Flutter Speed Limits of Cantilever Rectangular and Tapered Plates |
title_sort |
flutter speed limits of cantilever rectangular and tapered plates |
publisher |
Al-Khwarizmi College of Engineering – University of Baghdad |
publishDate |
2007 |
url |
https://doaj.org/article/fb501cf93cee4204b9d1680dbaa76265 |
work_keys_str_mv |
AT kusayhjabir flutterspeedlimitsofcantileverrectangularandtaperedplates |
_version_ |
1718400868098768896 |