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    Fundamental Consideration of Maximum Allowable Flaw Lengths for Limit Load Evaluation Based on Flat Plates for the ASME Code Section XI 

    Source: Journal of Pressure Vessel Technology:;2026:;volume( 148 ):;issue:004
    Author(s): Negyesi, Martin; Hasegawa, Kunio
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. When flaws are detected in power plants, they are evaluated to determine their impact on component integrity. Three conditions are imposed on the components in question to ensure they can operate safely. First, ...
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    Applicability of Instrumented Indentation for Assessing Allowable Flaw Sizes of Circumferentially Flawed Stainless Steel Piping 

    Source: Journal of Nondestructive Evaluation, Diagnostics and Prognostics of Engineering Systems:;2026:;volume( 009 ):;issue:003:;page 267
    Author(s): Ha, Yoosung; Negyesi, Martin; Hasegawa, Kunio; Lacroix, Valery
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. Structural integrity assessment of flawed pipes, as required by ASME B&PV Code Section XI, relies on failure stress calculated by the limit load criterion (LLC). The failure stress is derived from flow stress, ...
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    Development of Scaling Parameter SR for Negative Stress Ratios R Based on Trend in Experimental Data for Fatigue Crack Growth Rates of Austenitic Stainless Steels for ASME Code Section XI 

    Source: Journal of Pressure Vessel Technology:;2025:;volume( 147 ):;issue: 002:;page 21201-1
    Author(s): Negyesi, Martin; Yamaguchi, Yoshihito; Hasegawa, Kunio; Lacroix, Valery; Morley, Andrew
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Fatigue crack growth rates da/dN for stainless steels in air environment are provided by the ASME Code Section XI. The fatigue crack growth rates are given by da/dN = CF(ΔK)n, where CF is the fatigue crack growth rate ...
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