Flutter Phenomena Effected by The Aerodynamic Load

Flutter Phenomena Effected by The Aerodynamic Load

Abstract: The basic aim of this project is to define and investigate the flutter condition which occur at the wing and fuselage of the aircraft structure or any flying aerofoil such as engine fins during flight under different conditions and high speeds where the flutter causes a vibration on the wi...

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Bibliographic Details
Main Author: Abbass Salman
Format: Article
Language:English
Published: Unviversity of Technology- Iraq 2005-03-01
Series:Engineering and Technology Journal
Subjects:
ar aspect ratio- b chord length mm c / a length mid thickness to radius ratio ( thickness ratio ) cd drag coefficient cl lift coefficient cm moment coefficient cn normal force coefficient mm feli e modules of elasticity n/m2 fb bending freque
bt
ct) influence coefficient αº angle of attack degree θ the instantaneous angular displacement degree μ mass of the blade gm σ logarithmic decrement mm w eigen frequency rad\sec p air density kg / m3
Online Access:https://etj.uotechnology.edu.iq/article_181712_b27f51749292140d093da1edc8969121.pdf

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https://etj.uotechnology.edu.iq/article_181712_b27f51749292140d093da1edc8969121.pdf

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