Araştırma Makalesi

STRUCTURAL ANALYSIS AND OPTIMIZATION OF A FLAP MECHANISM OF AIRPLANES INTEGRATED WITH FEA SIMULATIONS

Cilt: 14 Sayı: 1 20 Mart 2026
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STRUCTURAL ANALYSIS AND OPTIMIZATION OF A FLAP MECHANISM OF AIRPLANES INTEGRATED WITH FEA SIMULATIONS

Öz

In this study, the flap mechanism of an aircraft was optimized by integrating its aerodynamic and structural behavior under operational conditions. First, a flow simulation was performed to obtain the pressure distribution on the flap surface and to calculate the resulting lift and drag forces. These aerodynamic loads were subsequently used as boundary conditions in a detailed finite element analysis to identify critical stress regions, deformation patterns, and load paths within the mechanism. Based on the structural response, topology optimization was applied to one of the primary components to reduce its weight while preserving the required strength and operational performance. The optimization process resulted in a substantial mass reduction of approximately 28.23% without compromising mechanical integrity. Overall, the findings of this study contribute to the development of more efficient, lightweight, and structurally reliable aircraft mechanisms.

Anahtar Kelimeler

Kaynakça

  1. Akçay, Ö., İlkılıç, C., 2025. Light-Weight Design of Aerospace Components Using Genetic Algorithm and Dandelion Optimization Algorithm. International Journal of Aeronautical and Space Sciences, 29(2), 2898–2909.
  2. Altınel, K., Yıldız, A., Yuce, C., 2023. Ağır ticari araç süspansiyon sistemleri için modüler taşıyıcı kol mekanizmasının tasarımı ve analizi. Gazi Üniversitesi Fen Bilimleri Dergisi Part C: Tasarım ve Teknoloji, 11(3), 794-803.
  3. Aydoğan, B., Yildiz, A., 2025. Mathematical modeling and optimization of the active suspension system of a 6×6 electric vehicle. Alexandria Engineering Journal, 127(8), 989-1003.
  4. Değirmencioğlu, F., Koşer, Y. C., Yildiz, A., 2023. Endüstriyel Robotlarda Kullanılan Çoklu Tutucunun Yapısal Analizi ve Optimizasyonu. Uluslararası Bilim Teknoloji ve Tasarım Dergisi, 4(2), 103-112.
  5. Elham, A., van Tooren, M.J.L., 2016. Coupled adjoint aerostructural wing optimization using quasi-three-dimensional aerodynamic analysis. Structural and Multidisciplinary Optimization, 54(4), 711-726. Elelwi, M., Botez, R. M., Dao, T.M., 2021. Structural Sizing and Topology Optimization Based on Weight Minimization of a Variable Tapered Span-Morphing Wing for Aerodynamic Performance Improvements. Biomimetics, 6(4), 55.
  6. Kavala Sen, D., Yildiz, A., Kopmaz, O., 2022. Optimal design of a five-bar planar manipulator and its controller by using different algorithms for minimum shaking forces and moments. Machines, 10(11), 971.
  7. Kayacan, M. Y., Alshihabi, M., 2024. Adaptive topology optimization for additive manufacturing in aerospace applications. Pamukkale University Journal of Engineering Sciences, 30(2), 145-154.
  8. Kenway, G.K.W., Martins, J.R.A., 2014. Multipoint high-fidelity aerostructural optimization of a transport aircraft configuration. Journal of Aircraft, 51(1), 144-160.

Ayrıntılar

Birincil Dil

İngilizce

Konular

Makine Teorisi ve Dinamiği

Bölüm

Araştırma Makalesi

Yayımlanma Tarihi

20 Mart 2026

Gönderilme Tarihi

24 Kasım 2025

Kabul Tarihi

14 Şubat 2026

Yayımlandığı Sayı

Yıl 2026 Cilt: 14 Sayı: 1

Kaynak Göster

APA
Erguvan, O., Erguvan, G., & Yıldız, A. (2026). STRUCTURAL ANALYSIS AND OPTIMIZATION OF A FLAP MECHANISM OF AIRPLANES INTEGRATED WITH FEA SIMULATIONS. Mühendislik Bilimleri ve Tasarım Dergisi, 14(1), 274-284. https://doi.org/10.21923/jesd.1828769
AMA
1.Erguvan O, Erguvan G, Yıldız A. STRUCTURAL ANALYSIS AND OPTIMIZATION OF A FLAP MECHANISM OF AIRPLANES INTEGRATED WITH FEA SIMULATIONS. MBTD. 2026;14(1):274-284. doi:10.21923/jesd.1828769
Chicago
Erguvan, Okan, Gökhan Erguvan, ve Ahmet Yıldız. 2026. “STRUCTURAL ANALYSIS AND OPTIMIZATION OF A FLAP MECHANISM OF AIRPLANES INTEGRATED WITH FEA SIMULATIONS”. Mühendislik Bilimleri ve Tasarım Dergisi 14 (1): 274-84. https://doi.org/10.21923/jesd.1828769.
EndNote
Erguvan O, Erguvan G, Yıldız A (01 Mart 2026) STRUCTURAL ANALYSIS AND OPTIMIZATION OF A FLAP MECHANISM OF AIRPLANES INTEGRATED WITH FEA SIMULATIONS. Mühendislik Bilimleri ve Tasarım Dergisi 14 1 274–284.
IEEE
[1]O. Erguvan, G. Erguvan, ve A. Yıldız, “STRUCTURAL ANALYSIS AND OPTIMIZATION OF A FLAP MECHANISM OF AIRPLANES INTEGRATED WITH FEA SIMULATIONS”, MBTD, c. 14, sy 1, ss. 274–284, Mar. 2026, doi: 10.21923/jesd.1828769.
ISNAD
Erguvan, Okan - Erguvan, Gökhan - Yıldız, Ahmet. “STRUCTURAL ANALYSIS AND OPTIMIZATION OF A FLAP MECHANISM OF AIRPLANES INTEGRATED WITH FEA SIMULATIONS”. Mühendislik Bilimleri ve Tasarım Dergisi 14/1 (01 Mart 2026): 274-284. https://doi.org/10.21923/jesd.1828769.
JAMA
1.Erguvan O, Erguvan G, Yıldız A. STRUCTURAL ANALYSIS AND OPTIMIZATION OF A FLAP MECHANISM OF AIRPLANES INTEGRATED WITH FEA SIMULATIONS. MBTD. 2026;14:274–284.
MLA
Erguvan, Okan, vd. “STRUCTURAL ANALYSIS AND OPTIMIZATION OF A FLAP MECHANISM OF AIRPLANES INTEGRATED WITH FEA SIMULATIONS”. Mühendislik Bilimleri ve Tasarım Dergisi, c. 14, sy 1, Mart 2026, ss. 274-8, doi:10.21923/jesd.1828769.
Vancouver
1.Okan Erguvan, Gökhan Erguvan, Ahmet Yıldız. STRUCTURAL ANALYSIS AND OPTIMIZATION OF A FLAP MECHANISM OF AIRPLANES INTEGRATED WITH FEA SIMULATIONS. MBTD. 01 Mart 2026;14(1):274-8. doi:10.21923/jesd.1828769