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SEDL / STP / STP1461-EB / STP11492S
Environmentally Influenced Fatigue in High Strength Steels
Lee, EU Materials Engineer, Naval Air Warfare Center Aircraft Division, Aerospace Materials Division, Patuxent River, MD
Vasudevan, AK Scientific Officer, Office of Naval Research, Arlington, VA
Pages: 13 Published: Jan 2005
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Abstract
A study was conducted to identify the environmental influence on fatigue crack growth behavior of three high strength steels: AerMet 100, 300M, and 4340. These steels were subjected to fatigue tests under constant amplitude loading of frequency 10 Hz and stress ratios R = 0.1 and 0.9, in vacuum, air, and 3.5% NaCl solution. The fatigue crack growth was characterized with two driving force parameters, stress intensity range, ΔK, and maximumCaret stress intensity, Kmax. Especially, the variation of fatigue crack growth per time, da/dt, with Kmax in 3.5% NaCl solution was evaluated with respect to R, environment, and threshold stress intensity for environmentally assisted cracking (EAC), KIEAC. In addition, the environmental influence on fatigue crack growth was examined with the fractographic features and trajectory path, drawn with the limiting values of ΔK and Kmax, ΔK* and Kmax*.
Keywords:
fatigue, environment, constant amplitude loading, frequency, stress ratio, environmentally assisted cracking (EAC), fractographic features, trajectory path
Paper ID: STP11492S
Committee/Subcommittee: E08.06
DOI: 10.1520/STP11492S
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