Effect Of Vibration Frequency On Naca 4412 Airfoil Aerodynamic Performance

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Effect Of Vibration Frequency On Naca 4412 Airfoil Aerodynamic Performance

Vibration is due to the aeroelastic stability of a typical section airplane wing NACA 4412 which finishes in general by the breaking of the plane, it can be determined as a dynamic instability of the structure. As vibration might lead to catastrophe, it is very important to understand the effect of...

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Bibliographic Details
Main Author:	Chan, Ze Yu
Format:	Monograph
Language:	English
Published:	Universiti Sains Malaysia 2019
Subjects:	T Technology
Online Access:	http://eprints.usm.my/58647/ http://eprints.usm.my/58647/1/Effect%20Of%20Vibration%20Frequency%20On%20Naca%204412%20Airfoil%20Aerodynamic%20Performance.pdf

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