Crack Propagation Behavior of Small Variable Load within Tensile Load Range

인장하중 범위내 작은 병동하중의 균열성장 거동

  • Published : 1998.10.01

Abstract

Fatigue crack propagation behavior for variable load in high strength aluminum alloys was investigated in this study. The materials used in this study are aluminum 7075-T651 and 5052-H32 alloys. Crack length was measured from calibration curve, which was plotted by known crack length and resistance of standard specimens. Load was obtained from linear regression formula. Unloading elastic compliance method was ap;ied to check the crack closure and cracked area.

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