[HTML][HTML] Strength-hardness relationship for AlSi10Mg alloy produced by laser powder bed fusion: An experimental study
A Serjouei, T Libura, A Brodecki… - Materials Science and …, 2022 - Elsevier
In this work, significant strength and ductility variations are reported for AlSi10Mg parts
fabricated at different orientations using laser powder bed fusion (LPBF). Hardness and …
fabricated at different orientations using laser powder bed fusion (LPBF). Hardness and …
Overcoming the strength-ductility trade-off dilemma in TiBw/TC18 composites via network architecture with trace reinforcement
In order to improve the ductility of TC18 (Ti–5Al–5Mo–5V–1Cr–1Fe) titanium alloy without
sacrificing its strength, TiBw/TC18 composites with low reinforcement content (≤ 2.0 vol%) …
sacrificing its strength, TiBw/TC18 composites with low reinforcement content (≤ 2.0 vol%) …
FEM based fatigue crack growth predictions for spar of light aircraft under variable amplitude loading
In the last decades, the assessment of the service durability of aerospace components and
assemblies has become an important segment of design, mostly because of the growing …
assemblies has become an important segment of design, mostly because of the growing …
Fatigue crack initiation and propagation behavior of nickel-based single crystal DD6 under different drilling processes
The fatigue crack initiation and propagation behavior of film cooling holes (FCHs) under
different drilling processes are of great significance to key structural parts. In this paper, it …
different drilling processes are of great significance to key structural parts. In this paper, it …
Failure analysis of an aircraft engine cylinder head
The piston engine of the training aircraft malfunctioned during the flight due to the cracking
of its cylinder head (CH), which is manufactured from an aluminum casting alloy. Based on …
of its cylinder head (CH), which is manufactured from an aluminum casting alloy. Based on …
[PDF][PDF] Aircraft duraluminum wing spar fatigue testing
N Petrašinović, D Petrašinović, B Rašuo… - FME …, 2017 - researchgate.net
Experimental fatigue crack growth analysis of the aircraft structural component subjected to
different cycling loading has been presented. The purpose of the experimental test was to …
different cycling loading has been presented. The purpose of the experimental test was to …
An investigation of the repetitive failure in an aircraft engine cylinder head
Cylinder head (CH) failures in aircraft piston engine may have serious or fatal
consequences to the safety of the crew and the aircraft. Moreover, when failure becomes …
consequences to the safety of the crew and the aircraft. Moreover, when failure becomes …
Extended finite element method (XFEM) applied to aircraft duralumin spar fatigue life estimation
D Petrašinović, B Rašuo, N Petrašinović - Tehnički vjesnik, 2012 - hrcak.srce.hr
Sažetak In the present work, duralumin aircraft spar fatigue life is evaluated by extended
finite element method (XFEM) under cyclic loading condition. The effect of the crack growth …
finite element method (XFEM) under cyclic loading condition. The effect of the crack growth …
[HTML][HTML] Approximate method for stress intensity factors determination in case of multiple site damage
A simple and easy to use approximate procedure, for calculating stress intensity factors, was
proposed. The procedure was developed based on existing solution for stress intensity …
proposed. The procedure was developed based on existing solution for stress intensity …
Practical aspects of finite element method applications in dentistry
A Grbović, D Mihajlović - Balkan Journal of Dental Medicine, 2017 - machinery.mas.bg.ac.rs
The use of numerical methods, such as finite element method (FEM), has been widely
adopted in solving structural problems with complex geometry under external loads when …
adopted in solving structural problems with complex geometry under external loads when …