Improving the aerodynamic stability of the plane wing cross-section using the method based on Fourier analysis
Publish place: 10th International Conference on Advanced Research in Science, Engineering and Technology
Publish Year: 1401
نوع سند: مقاله کنفرانسی
زبان: English
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شناسه ملی سند علمی:
RSETCONF10_099
تاریخ نمایه سازی: 28 شهریور 1401
Abstract:
In this paper, the aerodynamic stability of airplane wings was investigated by Fourier analysis. The effect of physical and geometrical parameters on the natural frequency, speed and flutter of the wings was investigated. Also, the aeroelastic analysis of the wing for the sweep angle of ۱۵ degrees and the free damping analysis for different flow regimes were performed.
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Authors
Ebrahim Hosseini
Department of mechanical engineering, Ahvaz Branch, Islamic Azad University, Ahvaz, Iran
Fatemeh Rezaeian
Department of Mathematics, Ahvaz Branch, Islamic Azad University, Ahvaz, Iran