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7075T73510合金断裂韧性和疲劳裂纹扩展 |
焦成革;候淑娥;李春玉;张禄山 |
北京航空材料研究所 |
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FRACTURE TOUGHNESS AND FATIGUE CRACK GROWTH RATE OF 7075T73510 ALLOY |
JIAO Chengge; HOU Shu'e; LI Chunyu; ZHANG Lushan (Institute of Aeronautical Materials; Beijing) |
引用本文:
焦成革;候淑娥;李春玉;张禄山. 7075T73510合金断裂韧性和疲劳裂纹扩展[J]. 材料研究学报, 1994, 8(1): 35-40.
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FRACTURE TOUGHNESS AND FATIGUE CRACK GROWTH RATE OF 7075T73510 ALLOY[J]. Chin J Mater Res, 1994, 8(1): 35-40.
1JackTelesman.NASATechnicalMemorandum,83636,1984,April:32HanGT,RosenfildAR.MetallTransA1975:6533AerospaceMaterialSpecificationAMS,4167E,1979:34ThompsonDS,ZinkhamRE.EngFracMech,1975;7(2):389 |
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