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1

Bakis, Charles E. Fatigue response of notched laminates subjected to tension-compression cyclic loads. Virginia Polytechnic Institute and State University, 1986.

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2

E, Melis Matthew, Halford Gary R, and United States. National Aeronautics and Space Administration., eds. Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip. National Aeronautics and Space Administration, 1990.

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3

E, Melis Matthew, Halford Gary R, and United States. National Aeronautics and Space Administration., eds. Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip. National Aeronautics and Space Administration, 1990.

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4

E, Melis Matthew, Halford Gary R, and United States. National Aeronautics and Space Administration., eds. Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip. National Aeronautics and Space Administration, 1990.

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5

Arya, V. K. Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip. National Aeronautics and Space Administration, 1990.

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6

A, Barrett C., Smith J, and NASA Glenn Research Center, eds. Long-term cyclic oxidation behavior of uncoated and coated Re108 and In939 at 980 and 870c̊. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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7

A, Barrett C., Smith J, and NASA Glenn Research Center, eds. Long-term cyclic oxidation behavior of uncoated and coated Re108 and In939 at 980 and 870c̊. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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8

A, Barrett C., Smith J, and NASA Glenn Research Center, eds. Long-term cyclic oxidation behavior of uncoated and coated Re108 and In939 at 980 and 870c̊. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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9

O, Harris David, Thomas Jerrell M, George C. Marshall Space Flight Center., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. A review of fracture mechanics life technology. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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10

United States. National Aeronautics and Space Administration., ed. Durability testing of commercial ceramic materials: Final report. National Aeronautics and Space Administration, 1996.

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11

United States. National Aeronautics and Space Administration., ed. Durability testing of commercial ceramic materials: Final report. National Aeronautics and Space Administration, 1996.

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12

Leonovich, Sergey, Evgeniy Shalyy, Elena Polonina, Elena Sadovskaya, Lev Kim, and Valentin Dorkin. Durability of port reinforced concrete structures (Far East and Sakhalin). INFRA-M Academic Publishing LLC., 2021. http://dx.doi.org/10.12737/1816638.

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Section I of the monograph is devoted to an urgent problem - forecasting the durability of port reinforced concrete structures, the destruction of which is associated with corrosion of steel reinforcement caused by chloride aggression and carbonation of concrete. The analysis of models for calculating the service life of structures and experimental data is carried out, the life cycles for the main degradation processes in concrete and reinforcement, the periods of initiation and propagation of corrosion are considered, the influence of environmental factors (temperature, humidity) and the qual
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13

K, Shaltens Richard, United States. Dept. of Energy. Office of Vehicle and Engine Research and Development., and Lewis Research Center, eds. Automotive Stirling summary and overview. National Aeronautics and Space Administation, Lewis Research Center, 1985.

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14

K, De Groh Kim, and Lewis Research Center, eds. Simulated solar flare X-ray and thermal cycling durability evaluation of Hubble Space Telescope thermal control candidate replacement materials. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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15

K, De Groh Kim, and Lewis Research Center, eds. Simulated solar flare X-ray and thermal cycling durability evaluation of Hubble Space Telescope thermal control candidate replacement materials. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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16

K, De Groh Kim, and Lewis Research Center, eds. Simulated solar flare X-ray and thermal cycling durability evaluation of Hubble Space Telescope thermal control candidate replacement materials. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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17

T, Long Sheila Ann, Long Edward R, and United States. National Aeronautics and Space Administration., eds. Studies of molecular properties of polymeric materials. Old Dominion University Research Foundation, 1990.

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18

T, Long Sheila Ann, Long Edward R, and Langley Research Center, eds. Studies of molecular properties of polymeric materials: Aerospace environmental effects on three linear polymers : final technical report for the period November 1, 1984 through October 31, 1985. Dept. of Physics, School of Sciences and Health Professions, Old Dominion University Foundation, 1985.

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19

Manson, S. S., and G. R. Halford. Fatigue and Durability of Structural Materials. ASM International, 2006. http://dx.doi.org/10.31399/asm.tb.fdsm.9781627083447.

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Fatigue and Durability of Structural Materials serves as a reference, textbook, and guide for engineers who design or maintain equipment subject to fatigue damage and failure. Using images, diagrams, and equations, it explains how cyclic loading affects the composition, structure, and properties of metals and the lifetime and performance of machine components. It describes the fundamentals of fatigue analysis, the role of dislocations, the concept of mean stress, the complexity of multiaxial loading, and the impact of cumulative fatigue damage. It discusses the influence of notches and cracks
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20

Manson, S. S., and G. R. Halford. Fatigue and Durability of Metals at High Temperatures. ASM International, 2009. http://dx.doi.org/10.31399/asm.tb.fdmht.9781627083430.

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Fatigue and Durability of Metals at High Temperatures is a repository of knowledge, experience, and insights on high-temperature fatigue and its effect on component lifetime and failure. The first few chapters provide readers with an intuitive understanding of creep and creep-fatigue and how they progress based on time, temperature, and stress. In subsequent chapters, the authors present several fatigue life prediction techniques, comparing them to each other and to experimental test results. The authors focus on a method called strain-range partitioning that breaks stress-strain hysteresis lo
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21

Long-term cyclic oxidation behavior of uncoated and coated Re108 and In939 at 980 and 870c̊. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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22

Durability testing of commercial ceramic materials: Final report. National Aeronautics and Space Administration, 1996.

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23

Simulated solar flare X-ray and thermal cycling durability evaluation of Hubble Space Telescope thermal control candidate replacement materials. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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24

Frank, Collins, and édéric Blin. Ageing of Infrastructure: A Life-Cycle Approach. Taylor & Francis Group, 2018.

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25

Frank, Collins, and Frederic Blin. Ageing of Infrastructure. Taylor & Francis Group, 2020.

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26

Frank, Collins, and édéric Blin. Ageing of Infrastructure: A Life-Cycle Approach. Taylor & Francis Group, 2018.

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27

Frank, Collins, and édéric Blin. Ageing of Infrastructure: A Life-Cycle Approach. Taylor & Francis Group, 2018.

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28

Ageing of Infrastructure: A Life-Cycle Approach. Taylor & Francis Group, 2018.

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29

Life cycle assessment in the built environment. Spon Press, 2011.

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30

Sarja, Asko. Integrated Life Cycle Design of Structures. Taylor & Francis Group, 2002.

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31

Sarja, Asko. Integrated Life Cycle Design of Structures. Taylor & Francis Group, 2002.

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32

Sarja, Asko. Integrated Life Cycle Design of Structures. Taylor & Francis Group, 2019.

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33

Sarja, Asko. Integrated Life Cycle Design of Structures. Taylor & Francis Group, 2002.

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34

Performance Requirements for Navy Ships Exterior Topside Coatings. AMPP, 2023. https://doi.org/10.5006/ampp_sp21417-2023.

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Scope This standard provides guidelines for establishing minimum requirements for the protective coatings of ships exterior topsides and related structures exposed to the marine atmosphere. It covers coating materials, coating test protocol and acceptance criteria, surface preparation, coating application, quality assurance and control, and repair method. Rationale In the late nineties, the North Atlantic Treaty Organization (NATO)(1) navies were considering approaches to improve the durability and maintainability of major assets. The importance of surface preparation, application processes an
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35

Transmission, Distribution, and Renewable Energy Generation Power Equipment: Aging and Life Extension Techniques. Taylor & Francis Group, 2017.

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36

Chudnovsky, Bella H. Transmission, Distribution, and Renewable Energy Generation Power Equipment: Aging and Life Extension Techniques, Second Edition. Taylor & Francis Group, 2017.

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37

Chudnovsky, Bella H. Transmission, Distribution, and Renewable Energy Generation Power Equipment: Aging and Life Extension Techniques. Taylor & Francis Group, 2020.

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38

Integrated life cycle design of structures. Spon Press, 2002.

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