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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| Format: | Monograph |
| Language: | English |
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Universiti Sains Malaysia
2019
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| Online Access: | http://eprints.usm.my/58647/1/Effect%20Of%20Vibration%20Frequency%20On%20Naca%204412%20Airfoil%20Aerodynamic%20Performance.pdf |