Fatigue Life Analysis of Aluminum Alloy Notched Specimens under Non-Gaussian Excitation based on Fatigue Damage Spectrum
In this study, a non-Gaussian excitation acceleration method is proposed, using aluminum alloy notched specimens as a research object and measured acceleration signal of a certain airborne bracket, during aircraft flight as input excitations, based on the fatigue damage spectrum (FDS) theory. The ku...
Saved in:
Main Authors: | Kuanyu Chen, Guangwu Yang, Jianjun Zhang, Shoune Xiao, Yang Xu |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2021-01-01
|
Series: | Shock and Vibration |
Online Access: | http://dx.doi.org/10.1155/2021/6887951 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
FREQUENCY DOMAIN DAMAGE CALCULATION AND EXPERIMENTAL VERIFICATION OF NON-GAUSSIAN EXCITATION BASED ON GMM MODEL (MT)
by: XU Yang, et al.
Published: (2023-01-01) -
RESEARCH ON STAGED FATIGUE DAMAGE OF ALUMINUM ALLOY 6061-T6
by: GENG MeiLing, et al.
Published: (2021-01-01) -
STUDY ON FATIGUE LIFE IN FREQUENCY DOMAIN FOR BOGIE FRAME
by: ZHU Tao, et al.
Published: (2016-01-01) -
FATIGUE LIFE PREDICTION AND EXPERIMENTAL STUDY OF ALUMINUM ALLOY WHEEL HUB CONSIDERING DAMAGE ACCUMULATION (MT)
by: WANG ZhaoHua, et al.
Published: (2023-01-01) -
FATIGUE STRENGTH PREDICTION OF RAILWAY AXLE SPECIMEN WITH SURFACE NOTCH BY TCD
by: XU YouKun, et al.
Published: (2022-01-01)