Small Crack Growth Behavior in Long Life Regime Of Aluminum Alloy 2017
It is generally known that the fatigue phenomenon of non-ferrous metals such as aluminum alloys are somewhat different from those of carbon steels. For example, it has been said that the knee point of S-N curve and non-propagating cracks do not appear in these metals. However, the exact meaning of t...
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Veröffentlicht in: | Nihon Kikai Gakkai ronbunshū. A 1989/10/25, Vol.55(518), pp.2124-2129 |
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container_title | Nihon Kikai Gakkai ronbunshū. A |
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creator | WATANABE, Toshimi KAWACHI, Shunichi YAMADA, Kunihiro KUNIO, Takeshi |
description | It is generally known that the fatigue phenomenon of non-ferrous metals such as aluminum alloys are somewhat different from those of carbon steels. For example, it has been said that the knee point of S-N curve and non-propagating cracks do not appear in these metals. However, the exact meaning of these phenomenon still seems ambiguous growth behavior at the apparent fatigue limit (defined for N=2×107) and fatigue strength was investigated using aluminum alloy 2017 (aged and annealed). In annealed and aged aluminum alloys, non-propagating cracks can exist after repetition of (25)×107 stress cycles. This suggests the possibility of existence of fatigue limit even in aluminum alloys. |
doi_str_mv | 10.1299/kikaia.55.2124 |
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For example, it has been said that the knee point of S-N curve and non-propagating cracks do not appear in these metals. However, the exact meaning of these phenomenon still seems ambiguous growth behavior at the apparent fatigue limit (defined for N=2×107) and fatigue strength was investigated using aluminum alloy 2017 (aged and annealed). In annealed and aged aluminum alloys, non-propagating cracks can exist after repetition of (25)×107 stress cycles. 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However, the exact meaning of these phenomenon still seems ambiguous growth behavior at the apparent fatigue limit (defined for N=2×107) and fatigue strength was investigated using aluminum alloy 2017 (aged and annealed). In annealed and aged aluminum alloys, non-propagating cracks can exist after repetition of (25)×107 stress cycles. This suggests the possibility of existence of fatigue limit even in aluminum alloys.</abstract><pub>The Japan Society of Mechanical Engineers</pub><doi>10.1299/kikaia.55.2124</doi><tpages>6</tpages><oa>free_for_read</oa></addata></record> |
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source | J-STAGE Free; Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals |
subjects | Aluminum Alloy Fatigue Non-propagating Crack S-N Curve Small Crack |
title | Small Crack Growth Behavior in Long Life Regime Of Aluminum Alloy 2017 |
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