Comparison of Crack Growth Models and Crack Closure Effect

Article Properties
  • DOI (url)
    10.4028/www.scientific.net/amr.311-313.822
  • Publication Date
    2011/08/01
  • Journal
    Advanced Materials Research
  • Indian UGC (journal)
  • Refrences
    9
  • Wen Lin Liu Naval Aeronautical and Astronautical University
  • Ri Jie Yang Naval Aeronautical and Astronautical University
  • Zhi Tao Mu Naval Aeronautical Engineering Academy
  • Shu Yan Liu Naval Aeronautical and Astronautical University
  • Da Zhao Yu Naval Aeronautical and Astronautical University
Abstract
Cite
Liu, Wen Lin, et al. “Comparison of Crack Growth Models and Crack Closure Effect”. Advanced Materials Research, vol. 311-313, 2011, pp. 822-5, https://doi.org/10.4028/www.scientific.net/amr.311-313.822.
Liu, W. L., Yang, R. J., Mu, Z. T., Liu, S. Y., & Yu, D. Z. (2011). Comparison of Crack Growth Models and Crack Closure Effect. Advanced Materials Research, 311-313, 822-825. https://doi.org/10.4028/www.scientific.net/amr.311-313.822
Liu WL, Yang RJ, Mu ZT, Liu SY, Yu DZ. Comparison of Crack Growth Models and Crack Closure Effect. Advanced Materials Research. 2011;311-313:822-5.
Refrences
Title Journal Journal Categories Citations Publication Date
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Life Predictions for High Cycle Dynamic Components Using Damage Tolerance Journal of the American Helicopter Society 3 2004
Fatigue crack growth behavior of Al7050-T7451 attachment lugs under flight spectrum variation Theoretical and Applied Fracture Mechanics
  • Technology: Mechanical engineering and machinery
  • Technology: Engineering (General). Civil engineering (General): Mechanics of engineering. Applied mechanics
  • Technology: Mechanical engineering and machinery
  • Technology: Engineering (General). Civil engineering (General)
 3 2003
Scott C. Forth. An Evaluation of the Applicability of Damage Tolerance to Dynamic Systems. Presented at the 8th Joint NASA/FAA/DOD Aging Aircraft Conference Palm Springs, California, USA, January 31 through February 3, (2005).
R. Jones, L. Molent. Critical Review of the Generalised Frost-Dugdale Approach to Crack Growth in F/A-18 Hornet Structural Materials. DSTO-RR-0350(2010).