Fatigue Testing of Resonating One-way Double-stiffened Plate

Wen Guang Liu; Hong Lin He

doi:10.4028/www.scientific.net/AMR.479-481.2005

Paper Titles

The Influence of Rare Earth Oxide on the Structure and Properties of AgSnO2 Electrical Contact Materials
p.1986

The Influence of Blind-Hole Depth and Bore to Strain Energy Relief Coefficients-a Case Study
p.1993

Tangent Stiffness Matrix of Single-Layer Reticulated Shell’s Members with Rigid Ends
p.1997

Fatigue Life Reliability Analysis of Submarine Cone-Cylinder Shell
p.2001

Fatigue Testing of Resonating One-way Double-stiffened Plate
p.2005

The Compensation of Automatic Control System Based on MATLAB
p.2009

Study on Wind Load Performance for L Type Aerial Work Suspended Platform
p.2013

Structure Optimization and Strength Analysis of CBM Special Anti-Clogging Drainage Pump
p.2017

Equivalent Stress Linearization Method Based on Assessment Line of Nozzle-Cylinder Intersection
p.2022

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 479-481Fatigue Testing of Resonating One-way...

Fatigue Testing of Resonating One-way Double-stiffened Plate

Abstract:

Problems of vibration fatigue exist in the field of aeronautics and astronautics widespread, which endangered the safety and reliability for structures of aircraft. Vibration-exciter-based fatigue testing system was designed and a method for fatigue testing of the resonating structure was proposed. In test, natural frequency of the test pieces was tracked by the exciting frequency. Experiments are carried out for the typical components with different working condition. One is with given strain, and another is with given force. Results indicate that impacts of the strain amplitude, the damping, the natural frequency and the boundary conditions on vibration fatigue life are obviously.

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Advanced Materials Research (Volumes 479-481)

Pages:

2005-2008

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.479-481.2005

Citation:

Cite this paper

Online since:

February 2012

Authors:

Wen Guang Liu, Hong Lin He

Keywords:

Fatigue Test, One-Way Double-Stiffened Plate, Resonance

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] Q. H. Yao and X. Q. Yang: Design Manual of Acoustic Fatigue for Aircraft Structures (Press of Aviation Industry, Beijing China 1991)

Google Scholar

[2] W. G. Liu and G. P. Chen: Chinese Mechanical Engineering Vol. 21(2010), pp.2798-2802

Google Scholar

[3] T. J. George, J. Seidt, M. H. Shen, etc.: International Journal of Fatigue Vol. 26(2004), pp.477-486

Google Scholar

[4] D. H. Schlums, J. Dual: Fatigue and Fracture of Engineering Material and Structural Vol. 20(1997), pp.1051-1058

Google Scholar

[5] X. Sun, R. Horowitz and K. Komvopoulos: Journal of Dynamic Systems, Measurement, and Control Vol. 124(2002), pp.599-605

Google Scholar

[6] A. J. Dentsoras, E. P.Kouvaritakis: Engineering Fracture Mechanics Vol. 50(1995), pp.467-473

Google Scholar

[7] S. Wolfgang: roceeding of the seventh international symposium on the vibrations of continuous system: Zakopand, Poland (2009)

Google Scholar