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1

Carpinteri, Alberto. Mechanical damage and crack growth in concrete. Springer Netherlands, 1986. http://dx.doi.org/10.1007/978-94-009-4350-6.

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2

Ellyin, Fernand. Fatigue Damage, Crack Growth and Life Prediction. Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-009-1509-1.

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3

Ellyin, Fernand. Fatigue damage, crack growth, and life prediction. Chapman & Hall, 1997.

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4

Pete, Kantzos, Telesman Jack, and United States. National Aeronautics and Space Administration., eds. Fatigue crack growth and crack bridging in SCS-6/Ti-24-11. National Aeronautics and Space Administration, 1995.

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5

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. An assessment of fatigue damage and crack growth prediction techniques. AGARD, 1994.

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6

1950-, Harris Charles E., and Langley Research Center, eds. Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure. National Aeronautics and Space Administration, Langley Research Center, 1996.

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7

Castelli, Michael G. Characterization of damage progression in SCS-6/Timetal 21S [0]₄ under thermomechanical fatigue loadings. National Aeronautics and Space Administration, 1994.

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8

Wanhill, R. J. H. Damage tolerance property comparisons for 2000 and 8000 series aluminium plate alloys. National Aerospace Laboratory, 1995.

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9

C, Newman J., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Analysis and prediction of multiple-site damage (MSD) fatigue crack growth. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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10

C, Newman J., and Langley Research Center, eds. Methodology for predicting the onset of widespread fatigue damage in lap-splice joints. National Aeronautics and Space Administration, Langley Research Center, 1998.

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11

Carpinteri, Alberto. Mechanical damage and crack growth in concrete: Plastic collapse to brittle fracture. Springer Netherlands, 1986.

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12

Center, Langley Research, ed. A progressive damage methodology for residual strength predictions of center-crack tension composite panels. National Aeronautics and Space Administration, Langley Research Center, 1996.

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13

Naik, Rajiv A. Observations of fatigue crack initiation and damage growth in notched titanium matrix composites. National Aeronautics and Space Administration, Langley Research Center, 1990.

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14

Jozef Cornelis Walterus van Vroonhoven. Dynamic crack propagation in brittle materials: Analyses based on fracture and damage mechanics. Eindhoven University of Technology, 1996.

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15

E, Harris C., Morris D. H, and Langley Research Center, eds. Surface crack analysis applied to impact damage in a thick graphite/epoxy composite. National Aeronautics and Space Administration, Langley Research Center, 1988.

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16

United States. National Aeronautics and Space Administration., ed. Damage mechanisms and controlled crack propagation in a hot pressed silicon nitride ceramic. National Aeronautics and Space Administration, 1994.

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17

United States. National Aeronautics and Space Administration., ed. Damage mechanisms and controlled crack propagation in a hot pressed silicon nitride ceramic. National Aeronautics and Space Administration, 1994.

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18

United States. National Aeronautics and Space Administration., ed. Modeling the growth and interaction of fractures. National Aeronautics and Space Administration, 1991.

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19

United States. National Aeronautics and Space Administration., ed. Modeling the growth and interaction of fractures. National Aeronautics and Space Administration, 1991.

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20

Schra, L. Influence of gust spectrum variations on fatigue crack growth behaviour of damage tolerant aluminium-lithium sheet materials (NLR contribution to BREU 3250, Task 4). National Aerospace Laboratory, 1992.

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21

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. An assessment of fatigue damage and crack growth prediction techniques: Papers presented at the 77th Meeting of the AGARD Structures and Materials Panel, held in Bordeaux, France 29th-30th September 1993. AGARD, 1994.

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22

Advisory Group for Aerospace Research and Development. Structures and Materials Panel. Meeting,, ed. An assessment of fatigue damage and crack growth prediction techniques: Papers presented at the 77th Meeting of the AGARD Structures and Materials Panel, held in Bordeaux, France, 29th-30th September 1993. Agard, 1994.

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23

A, Skinn D., Wright Laboratory (Wright-Patterson Air Force Base, Ohio). Materials Directorate., and Purdue University. Center for Information and Numerical Data Analysis and Synthesis., eds. Damage tolerant design handbook: A compilation of fracture and crack growth data for high-strength alloys. CINDAS, Purdue University, 1994.

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24

C, Chamis C., Minnetyan L, and United States. National Aeronautics and Space Administration., eds. Computational simulation of damage progression of composite thin shells subjected to mechanical loads. National Aeronautics and Space Administration, 1996.

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25

C, Chamis C., Minnetyan L, and United States. National Aeronautics and Space Administration., eds. Computational simulation of damage progression of composite thin shells subjected to mechanical loads. National Aeronautics and Space Administration, 1996.

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26

E, Harris Charles, and United States. National Aeronautics and Space Administration., eds. Experimental verification of a progressive damage model for IM7/5260 laminates subjected to tension-tension fatigue. National Aeronautics and Space Administration, 1995.

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27

Dore, Amanda Louise. Effects of fibre volume fraction on tensile damage and fatigue crack growth in Titanium metal matrix composites. University of Birmingham, 1997.

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28

Center, Langley Research, ed. Experimental verification of a progressive damage model for composite laminates based on continuum damage mechanics. National Aeronautics and Space Administration, Langley Research Center, 1994.

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29

C, Chamis C., and United States. National Aeronautics and Space Administration., eds. Structural durability of damaged metallic panel repaired with composite patches. National Aeronautics and Space Administration, 1997.

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30

C, Chamis C., and United States. National Aeronautics and Space Administration., eds. Structural durability of damaged metallic panel repaired with composite patches. National Aeronautics and Space Administration, 1997.

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31

C, Driscoll R. M., Littlejohn G. S, Institution of Civil Engineers, and Building Research Establishment, eds. Has your house got cracks?: A homeowner's guide to subsidence and heave damage. 2nd ed. Institution of Civil Engineers and Building Research Establishment, 2002.

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32

Piascik, Robert S. The characteristics of fatigue damage in the fuselage riveted lap splice joint. National Aeronautics and Space Administration, Langley Research Center, 1997.

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33

H, Starnes James, Newman J. C, and Langley Research Center, eds. Development of advanced structural analysis methodologies for predicting widespread fatigue damage in aircraft structures. National Aeronautics and Space Administration, Langley Research Center, 1995.

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34

Fatigue Damage, Crack Growth and Life Prediction. Springer, 2011.

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35

Fatigue Damage, Crack Growth and Life Prediction. Springer Netherlands, 1996.

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36

Mechanical damage and crack growth in concrete: Plastic collapse to brittle fracture. M. Nijhoff, 1986.

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37

Mechanical damage and crack growth in concrete: Plastic collapse to brittle fracture. Springer, 2011.

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38

National Aeronautics and Space Administration (NASA) Staff. Surface Crack Analysis Applied to Impact Damage in a Thick Graphite-Epoxy Composite. Independently Published, 2018.

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39

A progressive damage methodology for residual strength predictions of notched composite panels. National Aeronautics and Space Administration, Langley Research Center, 1998.

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40

Effects of Ballistic Impact Damage on Fatigue Crack Initiation in Ti- 6Al-4V Simulated Engine Blades. Storming Media, 2000.

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41

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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42

Kent, Gordon. Damage Control. HarperCollins Publishers Ltd, 2006.

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43

Lewis, Jaqueline. I Think I Have a Crack in My Amor! ... How'd That Happen?: Information to Help You Identify Your Triggers and How to Repair the Damage They Cause to Your Spiritual Armor. Independently Published, 2020.

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44

Lewis, Jaqueline. I Think I Have a Crack in My Armor! ... . How'd That Happen?: Information to Help You Identify Your Triggers and How to Repair the Damage They Cause to Your Spiritual Armor. Independently Published, 2020.

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45

Kent, Gordon. Damage Control. HarperCollins Publishers Limited, 2005.

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46

Kent, Gordon. Damage Control. HarperCollins Publishers Ltd, 2006.

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47

Kent, Gordon. Damage Control. HarperCollins Publishers Limited, 2010.

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48

Has your House got Cracks?: A Homeowner's Guide to Subsidence and Heave Damage, 2nd edition. Thomas Telford Ltd, 2001. http://dx.doi.org/10.1680/hyhgc.30893.

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49

Littlejohn, G. S., R. M. C. Driscoll, and T. J. Freeman. Has Your House Got Cracks?: Second Edition: A Homeowner's Guide to Subsidence and Heave Damage. 2nd ed. Thomas Telford Services Ltd, 2003.

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50

Kemske, Bonnie. Kintsugi. Bloomsbury Publishing Plc, 2021. http://dx.doi.org/10.5040/9781789942743.

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A stunning book on kintsugi, the Japanese art of repairing broken pottery with precious metals to highlight its history beautifully. A broken pot is made whole again, and within its golden repair we see a world of meaning. Kintsugi is the art of embracing imperfection. In Western cultures, the aim of repair has been to make the broken item ‘as good as new’. Kintsugi on the other hand, is a Japanese art that leaves an obvious repair – one that may appear fragile, but which actually makes the restored ceramic piece stronger, more beautiful, and more valuable than before. Leaving clear, bold, vis
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