Thermal shock loading of operating pressure equipment is a common occurrence, particularly in thermal power stations. The tensile stresses that are produced at the surface of a heated component exposed to a rapid thermal down shock can be very high, particularly in the presence of stress concentrations such as an abrupt change in geometry. Repeated application of the thermal shocks may eventually lead to crack initiation and crack growth. In some cases these cracks lead to component failure while in other cases the cracks arrest at a harmless depth. The ability to use current codes and standards to describe this type of crack growth is particularly desirable. Unfortunately, thermal shock is a very complex transient situation with highly non-linear stress distributions and environmental effects that are not well described by some codes. This paper describes attempts to use the stress versus cycles curve (S-N curves) described in the ASME Boiler and Pressure Vessel code to predict crack initiation in a flat plate carbon steel specimen exposed to repeated thermal shock from temperatures below the creep range. The issue considered in this paper is how to estimate stresses in this complex situation for notched specimens. Modifications to the code are suggested where necessary to achieve the desired accuracy. (C) 2003 Elsevier B.V. All rights reserved.
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Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R ChinaAir Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R China
Pan, Xinlei
Li, Xiang
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Shi Jiazhuang Flying Coll PLA Airforce, Training Brigade 1, Shijiazhuang 050000, Hebei, Peoples R ChinaAir Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R China
Li, Xiang
Zhou, Liucheng
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Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R ChinaAir Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R China
Zhou, Liucheng
Feng, Xiaotai
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Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R ChinaAir Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R China
Feng, Xiaotai
Luo, Sihai
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Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R ChinaAir Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R China
Luo, Sihai
He, Weifeng
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Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R China
Xi An Jiao Tong Univ, Sch Mech Engn, Inst Aeronaut Engine, Xian 710049, Shaanxi, Peoples R ChinaAir Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R China
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Univ Leoben, Dept Mat Sci, Franz Josef Str 18, A-8700 Leoben, AustriaUniv Leoben, Dept Mat Sci, Franz Josef Str 18, A-8700 Leoben, Austria
Paps, Roman
Sevecek, Oldrich
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Brno Univ Technol, Inst Solid Mech Mechatron & Biomech, Fac Mech Engn, Tech 2, Brno 61669, Czech RepublicUniv Leoben, Dept Mat Sci, Franz Josef Str 18, A-8700 Leoben, Austria
Sevecek, Oldrich
Schlacher, Josef
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Univ Leoben, Dept Mat Sci, Franz Josef Str 18, A-8700 Leoben, AustriaUniv Leoben, Dept Mat Sci, Franz Josef Str 18, A-8700 Leoben, Austria
Schlacher, Josef
Bermejo, Raill
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Univ Leoben, Dept Mat Sci, Franz Josef Str 18, A-8700 Leoben, AustriaUniv Leoben, Dept Mat Sci, Franz Josef Str 18, A-8700 Leoben, Austria
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King Abdulaziz Univ, Fac Sci & Arts Khulais, Dept Math, Jeddah 21589, Saudi Arabia
Sohag Univ, Fac Sci, Dept Math, Sohag 82524, EgyptKing Abdulaziz Univ, Fac Sci & Arts Khulais, Dept Math, Jeddah 21589, Saudi Arabia
Abbas, Ibrahim A.
Zenkour, Ashraf M.
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King Abdulaziz Univ, Fac Sci, Dept Math, Jeddah 21589, Saudi Arabia
Kafrelsheikh Univ, Fac Sci, Dept Math, Kafr Al Sheikh 33516, EgyptKing Abdulaziz Univ, Fac Sci & Arts Khulais, Dept Math, Jeddah 21589, Saudi Arabia