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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1991, Vol. 12 ›› Issue (10): 541-543.

• 论文 • Previous Articles     Next Articles

CONDITIONS FOR THE CRACK-TIP RESIDUAL COMPRESSIVE STRESS VANISHING AND THEIR APPLICATION TO ESTIMATE OF THE OVERLOAD CUT-OFF RATIOS

Jiao Liang   

  1. The First Air-Force Aeronautical Engineering College of Chinese PLA
  • Received:1989-09-21 Revised:1990-02-11 Online:1991-10-25 Published:1991-10-25

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341