EFFECT OF THICKNESS ON FATIGUE CRACK GROWTH UNDER CONSTANT AMPLITUDE LOADING AND FLIGHT SIMULATION LOADING

S. J. Zhang;Y. G. Zhu;X. Y. Huang;S. L. Liu;H. Ouyang;Z. W. Yue;A. M. Luo

Journal of Aeronautical Materials ›› 1993, Vol. 13 ›› Issue (4) : 52-61.

PDF(676 KB)
PDF(676 KB)
Journal of Aeronautical Materials ›› 1993, Vol. 13 ›› Issue (4) : 52-61.

EFFECT OF THICKNESS ON FATIGUE CRACK GROWTH UNDER CONSTANT AMPLITUDE LOADING AND FLIGHT SIMULATION LOADING

    {{javascript:window.custom_author_en_index=0;}}
  • {{article.zuoZhe_EN}}
Author information +
History +

HeighLight

{{article.keyPoints_en}}

Abstract

{{article.zhaiyao_en}}

Key words

QR code of this article

Cite this article

Download Citations
{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 1993, 13(4): 52-61

References

References

{{article.reference}}

Funding

RIGHTS & PERMISSIONS

{{article.copyrightStatement_en}}
{{article.copyrightLicense_en}}
PDF(676 KB)

Accesses

Citation

Detail

Sections
Recommended

/