Aircraft Composite Structures Fatigue Durability Test Method

Yue Liang Chen; Yuan Ling Lei; Yong Zhang

doi:10.4028/www.scientific.net/AMR.941-944.1558

Paper Titles

Regularity of Decreasing Strength Limit at the Time of Concrete's Freeze-Thaw Cycling
p.1537

The Preparation and Tribological Properties of Graphite Fluoride
p.1544

Nonlinear Model and Numerical Solutions of Large Deformation of Functionally Graded Conical Shell
p.1548

Calculating Fatigue Life of Helicopter Composite Blades Based on the Residual Strength Theory
p.1552

Aircraft Composite Structures Fatigue Durability Test Method
p.1558

The Preparation and Performance Study of Thermal Insulating Materials with Diatomite
p.1562

Mechanical Response of Ping-Pong Racket to Different Hyperelastic Surface Materials
p.1566

Research on Grind-Hardening Process through Integration of Physical Experiments and Dynamic Simulation
p.1570

Hydrophobic Coating on Silicon Wafer by Use of Industrial Coating-Bar Process in Atmosphere Parameter
p.1577

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 941-944Aircraft Composite Structures Fatigue Durability...

Aircraft Composite Structures Fatigue Durability Test Method

Abstract:

The mechanism of injury and damage evolution of composite aircraft is complex, traditional methods fatigue test relies on a large number of structural durability test data, not only consume large, but limited applicability. In order to ensure the fatigue of composite structures validated statistically, this article describes the most common methods: Life scatter factor method, load enhancement factor method and ultimate strength method.

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Advanced Materials Research (Volumes 941-944)

Pages:

1558-1561

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.941-944.1558

Citation:

Cite this paper

Online since:

June 2014

Authors:

Yue Liang Chen, Yuan Ling Lei, Yong Zhang

Keywords:

Composite Material, Life Scatter Factor Method, Load Enhancement Factor Method, Structural Durability, Ultimate Strength Method

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] Sendeckyj GP. Fitting models to composite materials fatigue data. American society for testing and materials STP 734; 1981. p.245–60.

Google Scholar

[2] Whitehead RS, Kan, HP, Cordero R, Saether ES. Certiﬁcation testing methodology for composite structures: volume I – data analysis. Naval air development center report 87042-60 (DOT/FAA/CT-86-39); (1986).

Google Scholar

[3] Wong R, Abbott R. Durability & damage tolerance of graphite/epoxy honeycomb structures. In: Proceedings of the 34th international SAMPE symposium, Anaheim, California; (1990).

Google Scholar

[4] Shen Z, Zhang X J, et al. An introduction to design and verification for composite aircraft Structures [M]. Shang hai: Shanghai Jiao tong University Press, (2011).

Google Scholar

[5] Shen Z, Shi Y H, Li G M. Composites allowables and structural design allowables[R]. Fifth international Forum on commercial aircraft applications, Shanghai, 2011. 9. 19-20.

Google Scholar

[6] James Giancaspro, Winson Taam, Raymond Wong. Modified Joint Weibull approach to determine load enhancement factors. International Journal of Fatigue 31 (2009), 787-790.

DOI: 10.1016/j.ijfatigue.2008.03.005

Google Scholar

[7] Chen Y B, Wang H, Chen X H. Strength analysis of composite aircraft structures[M]. Shang hai: Shanghai Jiaotong University Press, 2011. (in Chinese).

Google Scholar

[8] Devore JL. Probability and statistics for engineering and the sciences. Pacific Grove [CA]: Brooks/Cole Publishing; (2000).

Google Scholar