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1

Berger, John R. Study of static and dynamic fracture using strain measurements. Boulder, Colo: U.S. Dept. of Commerce, National Institute of Standards and Technology, 1990.

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2

Martínez Pañeda, Emilio. Strain Gradient Plasticity-Based Modeling of Damage and Fracture. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-63384-8.

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3

Berger, John R. Study of static and dynamic fracture using strain measurements. Boulder, Colo: U.S. Dept. of Commerce, National Institute of Standards and Technology, 1990.

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4

Kitamura, Takayuki. A nonlinear high temperature fracture mechanics basis for strainrange partitioning. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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5

Kitamura, Takayuki. A nonlinear high temperature fracture mechanics basis for strainrange partitioning. Cleveland, Ohio: Lewis Research Center, 1989.

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6

Wong, Louis Man Chu. Effect of formation on local strain fields and fracture of paper. Ottawa: National Library of Canada, 1995.

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7

Tejchman, Jacek. Simulations of strain localization in plain and reinforced concrete with enhanced continuum models. Gdańsk: Wydawn. Politechniki Gdańskiej, 2010.

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8

Wong, A. K. On the application of the strain energy density theory in predicting crack initiation and angle of growth. Melbourne, Australia: Aeronautical Research Laboratories, 1986.

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9

Whyatt, J. K. Numerical exploration of shear-fracture-related rock bursts using a strain-softening constitutive law. Washington: U.S. Dept. of the Interior, Bureau of Mines, 1991.

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10

W, Dally James, ed. Experimental solid mechanics. Knoxville, Tenn: College House Enterprises, 2010.

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11

Hiser, A. L. A user's guide to the NRC's piping fracture mechanics data base (PIFRAC). Washington, DC: Division of Engineering, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1987.

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12

Hiser, A. L. A user's guide to the NRC's piping fracture mechanics data base (PIFRAC). Washington, DC: Division of Engineering, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1987.

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13

Salem, J. A. Fracture toughness of Si₃N₄ measurement with short bar chevron-notched specimens. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

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14

Li, Jian. Simplified data reduction methods for the ECT test for mode III interlaminar fracture toughness. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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15

Powers, Laurence James. A study of posterior composite resin dental restorative materials with special reference to the sorption of water and plane strain fracture toughness. Toronto: Faculty of Dentistry, University of Toronto, 1988.

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16

Moore, Andrew J. Strain analysis using ESPI applied to fracture mechanics. 1993.

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17

Pañeda, Emilio Martínez. Strain Gradient Plasticity-Based Modeling of Damage and Fracture. Springer, 2018.

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18

Pañeda, Emilio Martínez. Strain Gradient Plasticity-Based Modeling of Damage and Fracture. Springer, 2017.

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19

I, Trefilov V., and Instytut problem materialoznavstva (Akademii͡a︡ nauk Ukraïnsʹkoï RSR), eds. Deformat͡s︡ionnoe uprochnenie i razrushenie polikristallicheskikh metallov. Kiev: Nauk. dumka, 1987.

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20

C, Chamis C., Minnetyan L, and United States. National Aeronautics and Space Administration., eds. Prediction of composite laminate fracture: Micromechanics and progressive fracture. [Washington, D.C: National Aeronautics and Space Administration, 1996.

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21

Mindess, Sidney, and Surendra P. Shah. Cement-Based Composites : Volume 64: Strain Rate Effects on Fracture. University of Cambridge ESOL Examinations, 2014.

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22

R, Halford Gary, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. A nonlinear high temperature fracture mechanics basis for strainrange partitioning. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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23

I, Trefilov V., and Institut problem materialovedenii͡a︡ im. I.N. Frant͡s︡evicha., eds. Deformat͡s︡ionnoe uprochnenie i razrushenie polikristallicheskikh metallov. 2nd ed. Kiev: Nauk. dumka, 1989.

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24

Convergence of strain energy release rate components for edge-delaminated composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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25

Jacky, Mazars, Bažant Z. P, Centre national de la recherche scientifique (France), National Science Foundation (U.S.), and France-U.S. Workshop on Strain Localization and Size Effect Due to Cracking and Damage (1988 : Laboratoire de Mécanique et Technologie), eds. Cracking and damage: Strain localization and size effect. London: Elsevier Applied Science, 1989.

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26

Analytical studies of transverse strain effects on fracture toughness for circumferentially oriented cracks. Supt. of Docs., U.S. G.P.O. [distributor], 1991.

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27

Strain intensity factor approach for predicting the strength of continuously reinforced metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

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28

United States. National Aeronautics and Space Administration., ed. Analysis of delamination related fracture processes in composites. [Washington, DC: National Aeronautics and Space Administration, 1992.

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29

Mindess, Sidney. Cement-Based Composites: Strain Rate Effects on Fracture : Symposium (Materials Research Society Symposium Proceedings). Materials Research Society, 1986.

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30

R, Seshadri B., and Langley Research Center, eds. Fracture analysis of the FAA/NASA wide stiffened panels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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31

An evaluation of the fatigue crack growth and fracture toughness properties of beryllium-copper alloy CDA172. Houston, Tex: National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1990.

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32

A back face strain compliance expression for the compact tension specimen. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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33

S, Piascik Robert, and Langley Research Center, eds. A back face strain compliance expression for the compact tension specimen. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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34

United States. National Aeronautics and Space Administration., ed. Analysis of delamination related fracture processes in composites: Semi-annual report. [Washington, DC: National Aeronautics and Space Administration, 1992.

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35

United States. National Aeronautics and Space Administration, ed. Analysis of delamination related fracture processes in composites: Preliminary final report. [Washington, DC: National Aeronautics and Space Administration, 1988.

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36

United States. National Aeronautics and Space Administration., ed. Analysis of delamination related fracture processes in composites: Preliminary final report. [Washington, DC: National Aeronautics and Space Administration, 1988.

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37

Nagl, Michael Martin. Identification of the mechanism of oxide scale fracture, and its correlation with strain using acoustic emission. 1992.

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38

J, Minguet Pierre, O'Brien T. Kevin, and Langley Research Center, eds. A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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39

A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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40

Center, Langley Research, ed. Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material. Hampton, Va: National Aeronautics and Science Administration, Langley Research Center, 2001.

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41

Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material. Hampton, Va: National Aeronautics and Science Administration, Langley Research Center, 2001.

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42

Sidney, Mindess, Shah S. P, and Materials Research Society, eds. Cement-based composites: Strain rate effects on fracture : symposium held December 4-5, 1985, Boston, Massachusetts, USA. Pittsburgh, Pa: Materials Research Society, 1986.

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43

S, Raju I., O'Brien T. Kevin, and Langley Research Center, eds. Strain-energy-release rate analysis of the end-notched flexure specimen using the finite-element method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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44

S, Raju I., O'Brien T. Kevin, and Langley Research Center, eds. Strain-energy-release rate analysis of the end-notched flexure specimen using the finite-element method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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45

S, Raju I., O'Brien T. Kevin, and Langley Research Center, eds. Strain-energy-release rate analysis of the end-notched flexure specimen using the finite-element method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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46

Modeling of stress/strain behavior of fiber-reinforced ceramic matrix composites including stress redistribution. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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47

MODELING OF HIGH-STRAIN-RATE DEFORMATION, FRACTURE, AND IMPACT BEHAVIOR OF ADVANCED GAS TURBINE ENGINE MATERIALS..., NASA/CR--2003-212194... [S.l: s.n., 2003.

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48

Analysis of interface crack branching. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.

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49

David, Nathenson, Prakash Vikas, and NASA Glenn Research Center, eds. Modeling of high-strain-rate deformation, fracture, and impact behavior of advanced gas turbine engine materials at low and elevated temperatures. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

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50

David, Nathenson, Prakash Vikas, and NASA Glenn Research Center, eds. Modeling of high-strain-rate deformation, fracture, and impact behavior of advanced gas turbine engine materials at low and elevated temperatures. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

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