서지주요정보
Al-Zn-Mg 합금에서 center notched specimen 을 이용한 부식피로 균열 전파 거동에 대한 속도론적인 연구 = Kinetics of corrosion fatigue crack propagation behaviour of Al-Zn-Mg alloy using a center notched specimen
서명 / 저자 Al-Zn-Mg 합금에서 center notched specimen 을 이용한 부식피로 균열 전파 거동에 대한 속도론적인 연구 = Kinetics of corrosion fatigue crack propagation behaviour of Al-Zn-Mg alloy using a center notched specimen / 장진영.
발행사항 [서울 : 한국과학기술원, 1986].
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4104057

소장위치/청구기호

학술문화관(문화관) 보존서고

MMS 8646

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Kinetics of corrosion fatigue (CF) crack propagation behaviour of Al-Zn-Mg alloy have been studied as a function of applied potential and temperature in 3.5 wt% NaCl solution using a center notched specimen. CF tests were carried out over a range of temperature from 303 to 348 K and over a range of applied potential -840 to -640 $mV_{SHE}$ with a loading frequency of 3 cpm. Stress-corrosion cracking (SCC) tests were also carried out in 3.5 wt% NaCl solution using a center notched specimen to validate superposition model. A continuously recording electrical potential system was used for monitering crack propagation. CF crack as well as stress-corrosion (SC) crack propagated in intergranular mode, irrespective of temperature and applied potential. This is due to low loading frequency. Since there were similarities in applied potential dependence of CF and SC crack propagation and in CF and SCC fracture surfaces, CF crack propagation was thought to be enhanced by SC crack propagation caused due to dynamic straining at a crack tip during CF. CF crack propagation rate, $(da/dN)_{CF}$, is the sum of three components - the fatigue crack propagation rate in a inert environment, $(da/dN)_{F}$, which represents the contribution of pure fatigue, a cycle-dependent component, $(da/dN)_{cf}$, that requires the synergistic interaction of fatigue and environmental attack, and the contribution by SCC, $(da/dN)_{scc}$. Apparent activation energy for CF crack propagation process was found to be about 52 kJ/mole at corrosion potential and independent of stress intensity factor range. CF crack propagation rate was proportional to the square of stress intensity factor range and was expressed as follows $(da/dN)_{CF} = A (\Delta K)^2 exp(-Q/RT)$ A equation for crack propagation rate was equivalent to the equation for hydrogen embrittlement crack propagation rate derived by H.W. Liu. It is suggested on the basis of CF and SCC fracture surface observation and dependence of CF crack propagation rate on the stress intensity factor range that CF crack propagation is caused by hydrogen embrittlement.

서지기타정보

서지기타정보
청구기호 {MMS 8646
형태사항 [iii], 65 p. : 삽화 ; 26 cm
언어 한국어
일반주기 저자명의 영문표기 : Jin-Young Jang
지도교수의 한글표기 : 변수일
지도교수의 영문표기 : Su-Il Pyun
학위논문 학위논문(석사) - 한국과학기술원 : 재료공학과,
서지주기 참고문헌 : p. 35-40
주제 Aluminum alloys.
Fatigue.
Dynamics.
알루미늄 합금. --과학기술용어시소러스
부식 피로. --과학기술용어시소러스
균열 전파. --과학기술용어시소러스
속도론. --과학기술용어시소러스
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