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RISSThe objective of this thesis is to investigate the influence of welding residual stresses on the fatigue growth behavior of cracks located transverse to the weld bead. For this purpose, G.T.A. (Gas Tungsten Arc) welding was performed on the AI. Alloy ...
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RISS 인기검색어
알루미늄 합금 용접부의 피로강도 평가에 대한 연구 = A Study on the Fatigue Strength Evaluation in Aluminum Alloy Weldments
한글로보기https://www.riss.kr/link?id=A75066445
- 저자
- 발행기관
- 학술지명
- 권호사항
-
발행연도
1995
-
작성언어
Korean
-
주제어
알루미늄 ; 합금 ; 용접부 ; 피로강도 ; Fatigue Strength ; Evaluation ; Aluminum
-
KDC
500
-
자료형태
학술저널
-
수록면
105-120(16쪽)
- 제공처
-
0
상세조회 -
0
다운로드
부가정보
다국어 초록 (Multilingual Abstract)
The objective of this thesis is to investigate the influence of welding residual stresses on the fatigue growth behavior of cracks located transverse to the weld bead. For this purpose, G.T.A. (Gas Tungsten Arc) welding was performed on the AI. Alloy 1100-O plate and the same initial crack is made on HAZ(Heat Affected Zone), weld metal and base metal respectively.
C.T.(Compact Tension) specimens were used as experimental material. Initial welding residual stresses were measured by using strain gage sectioning method. All specimens were tested under constant amplitude load with stress ratio R=0.1.
C.T.(Compact Tension) specimens were used as experimental material. Initial welding residual stresses were measured by using strain gage sectioning method. All specimens were tested under constant amplitude load with stress ratio R=0.1.
The objective of this thesis is to investigate the influence of welding residual stresses on the fatigue growth behavior of cracks located transverse to the weld bead. For this purpose, G.T.A. (Gas Tungsten Arc) welding was performed on the AI. Alloy 1100-O plate and the same initial crack is made on HAZ(Heat Affected Zone), weld metal and base metal respectively.
C.T.(Compact Tension) specimens were used as experimental material. Initial welding residual stresses were measured by using strain gage sectioning method. All specimens were tested under constant amplitude load with stress ratio R=0.1.
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