Introduction of Developing Fatigue Load Spectrum for Full-Scale Fatigue Test of Composite Aircraft-Reference-Cited by-同舟云学术

Introduction of Developing Fatigue Load Spectrum for Full-Scale Fatigue Test of Composite Aircraft

Published:2020-02-14 Issue:3 Volume:21 Page:681-692
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Joo Young-Sik,Lee Won-Jun,Seo Bo-Hwi,Lim Seung-Gyu

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Link

http://link.springer.com/content/pdf/10.1007/s42405-020-00257-8.pdf

Reference10 articles.

1. Broek D, Smith SH, Rice RC (1991) Generation of spectra and stress histories for fatigue and damage tolerance analysis of fuselage repair, DOT-VNTSC-FAA-91-16, pp 8–15

2. CMH-17-3G (2002) Composite materials handbook, vol 3, pp 64–100

3. Joo YS, Lee WJ, Seo BH, Lim SG (2019) A study on statistical characteristics of fatigue life of carbon fiber composite. JKSAS 47(1):35–40

4. Joo YS, Lim SG (2018) Evaluation of fatigue life and properties in composite material. In: KIMST conference proceedings

5. Sendeckyj GP (1981) Fitting models to composite materials fatigue data. ASTM STP 734:245–260

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