Development of a prediction model using fully connected neural networks in the analysis of composite structures under bird strike

2022-02-01
Hasilci, Zehra
BOĞOÇLU, Muharrem Erdem
DALKILIÇ, Ahmet Selim
Kayran, Altan
Bird strike is one of the most hazardous issues facing global aviation. In the present study, a hybrid methodology is developed utilizing, automated data generation and fully connected neural networks to practically and reliably obtain the global deformation of composite structures subject to bird strike. The validation of the proposed numerical bird strike model is accomplished by making comparisons with the available experimental data from three different resources in the literature on the chicken and gelatine strike tests to a rigid plate, and strike test against an aircraft composite vertical leading edge. For three different bird velocities, 9402 input files are created by an automatic data generator considering all possible stacking sequence combinations in accordance with the composite design guidelines. The global deformation of composite laminates caused by bird strike is estimated via the fully connected neural networks established. Results of the present study show that with the use of fully connected neural networks, global deformation of the composite laminate can be estimated reliably and preliminary design of the composite laminate can be performed very fast compared to performing nonlinear finite element analysis involving bird strike. In conclusion, the fully connected neural network model is found to be an alternative for additional LS-Dyna simulations in the optimization process.
JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY

Suggestions

Investigation of effects of bird strike problem on wing leading edge by using explicit finite element method
Dede, Oğuzhan; Kayran, Altan; Department of Aerospace Engineering (2015)
In aviation industry, bird strike problem causes structural damage and threats to flight safety. Nowadays, designed and produced aircraft have to satisfy “safe flight and landing” requirements. The behavior of the aircraft components during bird strike have be to investigated by numerical methods or experiments. Results obtained from numerical analysis and /or experiments have to be carefully studied to optimize the aircraft structures. However, experiments of bird strike are very costly and require qualifi...
Investigation of effects of bird strike on wing leading edge by using explicit finite element method
Dede, Oğuzhan; Kayran, Altan (null; 2015-09-10)
In aviation industry, bird strike problem causes structural damage and threats to flight safety. Nowadays, designed and produced aircraft have to satisfy “safe flight and landing” requirements. The behavior of the aircraft components during bird strike have to be investigated by numerical methods or experiments. Results obtained from numerical analysis and /or experiments have to be carefully studied to optimize the aircraft structures. The main aim of this study is to apply the explicit finite element anal...
Analysis of a UAV that can Hover and Fly Level
Cakici, Ferit; Leblebicioğlu, Mehmet Kemal (EDP Sciences; 2016-03-14)
In this study, an unmanned aerial vehicle (UAV) with level flight, vertical take-off and landing (VTOL) and mode-changing capability is analysed. The platform design combines both multirotor and fixed-wing (FW) conventional airplane structures and control surfaces; therefore, named as VTOL-FW. The aircraft is modelled using aerodynamical principles and linear models are constructed utilizing small perturbation theory for trim conditions. The proposed method of control includes implementation of multirotor a...
Investigation of rotor rotor interactions for two helicopters in forward flight using free vortex wake methodology
Tonkal, Ozan Çağrı; Pehlivan, Sercan; Sezer Uzol, Nilay; İşler, Veysi (null; 2010-07-01)
This paper presents an investigation of the aerodynamic interactions between two UH-1H helicopter rotors in forward flight. The wake flow structure and performance characteristics of the rotors are investigated when the rear rotor is operating within the wake of the front rotor. A 3-D unsteady vortex-panel method potential flow solver based on a free-vortex-wake methodology is used for this purpose. The solver is validated using the experimental data from the Caradonna-Tung experiments. The interactional an...
Development and implementation of novel flow control techniques for nonslender delta wings
Çelik, Alper; Yavuz, Mehmet Metin; Department of Mechanical Engineering (2017)
Understanding and controlling the physical phenomenon behind the aerodynamics of low to moderate swept delta wings has been a challenge for researchers during the last few decades, which is stimulated by their widespread use in unmanned combat air vehicles (UCAVs) and micro air vehicles (MAVs). Although delta wings are capable of generating high lift and stable flight performance at high angle of attack, the problems related to lack of conventional flow control surfaces compel the researchers to explore new...
Citation Formats
Z. Hasilci, M. E. BOĞOÇLU, A. S. DALKILIÇ, and A. Kayran, “Development of a prediction model using fully connected neural networks in the analysis of composite structures under bird strike,” JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY, pp. 0–0, 2022, Accessed: 00, 2022. [Online]. Available: https://hdl.handle.net/11511/96034.