Computational methods for bird strike simulations: A review

S Heimbs - Computers & Structures, 2011 - Elsevier
Bird strikes are a major threat to aircraft structures, as a collision with a bird during flight can
lead to serious structural damage. Computational methods have been used for more than 30 …

A stabilized SPH method for inviscid shallow water flows

R Ata, A Soulaïmani - … journal for numerical methods in fluids, 2005 - Wiley Online Library
In this paper, the smoothed particle hydrodynamics (SPH) method is applied to the solution
of shallow water equations. A brief review of the method in its standard form is first described …

Finite element modeling of a bird striking an engine fan blade

RH Mao, SA Meguid, TY Ng - Journal of Aircraft, 2007 - arc.aiaa.org
FAA statistical data reveal that gas turbine engines are the most vulnerable to bird strikes. In
reality, almost all severe accidents are closely related to the failure of the engines, which are …

Transient three dimensional finite element analysis of a bird striking a fan blade

RH Mao, SA Meguid, TY Ng - … Journal of Mechanics and Materials in …, 2008 - Springer
A comprehensive three-dimensional nonlinear finite element analyses were carried out to
examine the effects of the geometry and the incidence angle of canonical 4-lb bird striking a …

Numerical simulation of bird impact on hollow blades of titanium fan assembly

N Hou, Y Li, J Liu - Journal of Aerospace Engineering, 2019 - ascelibrary.org
In this paper, a bird impact test was carried out on a static hollow blade, and a numerical
model corresponding to the test was established based on the dynamic explicit finite …

Effects of incidence angle in bird strike on integrity of aero-engine fan blade

RH Mao, SA Meguid, TY Ng - International Journal of …, 2009 - Taylor & Francis
The possibilities of blade deformation and even fracture, the need for subsequent
containment and reduction in thrust and power supply make bird strikes to aero-engine fan …

[HTML][HTML] 航空发动机风扇叶片鸟撞研究进展

刘永泉, 罗刚, 张海洋, 陈伟 - 航空动力学报, 2024 - jasp.com.cn
综述了自20 世纪末至今以来航空发动机风扇叶片鸟撞问题在鸟体几何选型与建模,
瞬态动力学数值分析方法, 叶片鸟撞响应与损伤以及鸟撞关键试验技术等方面的进展, 结果表明 …

Full SPH fluid–shell interaction for leakage simulation in explicit dynamics

B Maurel, S Potapov, J Fabis… - International journal for …, 2009 - Wiley Online Library
This paper is devoted to the modeling of fluid leakage through a shell in case of impact
loading. The modeling of the fluid and the shell is based on SPH formulation. The proposed …

Failure analysis of rotorcraft composite end plate structure under high-velocity bird impact

RV Kumar - Journal of Failure Analysis and Prevention, 2016 - Springer
The paper discusses finite element (FE) modeling for predicting structural damage and
correlation studies of dynamic responses in rotorcraft composite structures under high …

Helicopter main rotor blade root end under high velocity bird impact

DC Naik, RV Kumar - Materials Today: Proceedings, 2018 - Elsevier
A numerical simulation methodology has been successfully developed to model the bird
strike on the innovative helicopter main rotor blade root end under high velocity bird impact …