Results 41 to 50 of about 242,308 (112)

Study on high-low cycle fretting fatigue life of Inconel718 tenon structure

Hangkong gongcheng jinzhan
The turbine blades of aero-engines are subjected to cyclic high-low cycle loads in actual service environments，which is a typical high-low cycle micro motion fatigue condition. The frequent occurrence of fatigue fracture in turbine blades due to fretting
YANG Xiaolin, MU Qinqin, CHEN Yonghui, YAN Qun   +3 more
doaj   +1 more source

Acoustic emission characterization of sliding wear under condition of direct and inverse transformations in low-temperature degradation aged Y-TZP and Y-TZP-AL2O3

Friction, 2018
In this research, results of the investigation of the sliding friction and wear of yttria-stabilized tetragonal zirconia polycrystalline (Y-TZP) and Y-TZP-Al2O3 samples preliminarily subjected to low-temperature degradation are reported.
Nikolai L. Savchenko, Andrey V. Filippov, Sergei Yu Tarasov, Andrey I. Dmitriev, Evgeny V. Shilko, Aleksandr S. Grigoriev   +5 more
doaj   +1 more source

Ground Strength Test Technique of Variable-Camber Wing Leading Edge

Biomimetics
Morphing wing technology is crucial for enhancing the flight performance of aircraft. To address the monitoring challenges of full-scale variable-camber leading edges under flight conditions, this study introduces a ground-based strength testing ...
Shanshan Li, Xianmin Chen, Zhigang Wang, Yuanbo Liang   +3 more
doaj   +1 more source

Post-Buckling Failure Mechanism and Optimal Tapered Termination Design for Composite Hat-Stiffened Panels

Aerospace
Composite hat-stiffened panels are widely used in civil aircraft structural design as typical closed-section stiffened components with high load-carrying efficiency.
Guofan Zhang, Chunhua Wan, Liang Chang, Xiaohua Nie   +3 more
doaj   +1 more source

NUMERICAL STUDY OF STRESS-STRAIN LOCALIZATION IN THE TITANIUM SURFACE MODIFIED BY AN ELECTRON BEAM TREATMENT

Facta Universitatis. Series: Mechanical Engineering, 2016
Numerical simulation is performed to investigate the mesoscale stress-strain localization in a surface-modified commercial titanium alloy. The calculated crystalline microstructure corresponds to that observed in experiments and is accounted for in an ...
Ruslan Balokhonov, Varvara Romanova, Alexey Panin, Sergey Martynov, Marina Kazachenok   +4 more
doaj   +1 more source

Study on the Dynamic Mechanical Behavior of 2D C/SiC Composites at Medium Strain Rates

Aerospace
Two-dimensional C/SiC are promising candidates for use in high-temperature structures in aeroengines and thermal protection systems in the aerospace industry, which will be subjected to loads in various directions during service.
Xinyue Zhang, Chao Zhang, Xiaochuan Liu, Chunyu Bai, Xulong Xi, Xiaocheng Li   +5 more
doaj   +1 more source

One Kind of Green New Method for Detection of Inside Layer Cracks of Aircraft Multilayer Structures

Engineering Proceedings
To address the technical challenges in detecting internal cracks within aircraft metallic multilayer structures, we have employed the environmentally friendly detection technique of remote-field eddy current (RFEC).
Huabin Huang, Zhiwei Peng, Mao Xu
doaj   +1 more source

Digital collaborative exploration and practice of ground vibration test for full-scale aircraft

Hangkong gongcheng jinzhan
The ground vibration test of full-scale aircraft has the characteristics of multiple coordination units, complex system, long implementation time and high risk.
BAI Chunyu, LIANG Sen, SONG Qiaozhi
doaj   +1 more source

Prediction of Random Crack Propagation Life of Thin Porous Plate with Multiple Site Damage

Engineering Proceedings
Based on the crack propagation rate test of LY12CZ aluminum alloy flat plate, the distribution characteristics of Paris formula parameters were characterized by the three-parameter logarithmic normal distribution, and a LY12CZ random crack propagation ...
Hanbin Sun, Xianmin Chen, Jun Yang
doaj   +1 more source

Strength

Arthroplasty Today, 2023
openaire   +3 more sources