An equilibrium multi-objective optimum design for non-circular clearance hole of disk with discrete variables-Reference-Cited by-同舟云学术

An equilibrium multi-objective optimum design for non-circular clearance hole of disk with discrete variables

Published:2018-02 Issue:2 Volume:31 Page:247-254
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

HAN Jiaxin,GUO Haiding

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference25 articles.

1. Connecting techniques of the modern long life aircraft;Yuan;J Eng Technol,2002

2. Strength and fatigue life calculation of an engine turbine disk;Ye;J Aeroeng,2006

3. Aviation engine structure design and analysis;Chen,2006

4. Structural optimization of uniaxial symmetry non-circular bolt clearance hole on turbine disk;Chen;Chin J Aeronaut,2014

5. Zhang C. Stress field analysis and structural optimization of non-circular hole on flange of turbine disks [dissertation]. Nanjing: Nanjing University of Aeronautics and Astronautics; 2014 [Chinese].

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Stress Optimization of Vent Holes with Different Shapes Using Efficient Switching Delayed PSO Algorithm;Applied Sciences;2022-05-26

2. Crystal plasticity analysis of temperature-sensitive dwell fatigue in Ti-6Al-4V titanium alloy for an aero-engine fan disc;International Journal of Fatigue;2022-03

3. Optimal location and shape definition of elliptical ventilation openings on aero engine turbine rotors with stress concentration effect;Chinese Journal of Aeronautics;2022-01

4. Effect of cold expansion on high-temperature low-cycle fatigue performance of the nickel-based superalloy hole structure;International Journal of Fatigue;2021-10