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1

1925-, Riley William F., ed. Experimental stress analysis. 3rd ed. New York: McGraw-Hill, 1991.

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2

1925-, Riley William F., ed. Experimental stress analysis. 3rd ed. New York: McGraw-Hill, 1991.

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3

Ling, Hoe I., Luigi Callisto, Dov Leshchinsky, and Junichi Koseki, eds. Soil Stress-Strain Behavior: Measurement, Modeling and Analysis. Dordrecht: Springer Netherlands, 2007. http://dx.doi.org/10.1007/978-1-4020-6146-2.

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4

Freed, Alan David. On the thermodynamics of stress rate in the evolution of back stress in viscoplasticity. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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5

Formulas for stress, strain, and structural matrices. 2nd ed. Hoboken, NJ: John Wiley & Sons, 2005.

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6

Formulas for stress, strain, and structural matrices. New York: J. Wiley, 1994.

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7

Verderaime, V. Test load verification through strain data analysis. Washington, DC: National Aeronautics and Space Administration, 1995.

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8

Hwang, C. Robin. Computer aided analysis of the stress/strain response of high polymers. Edited by Lin Chiah C, Matis Gary, and Hopfe H. H. Lancaster, PA: Technomic, 1989.

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9

Keil, Stefan. Technology and Practical Use of Strain Gages With Particular Consideration of Stress Analysis Using Strain Gages. Berlin, Germany: Wilhelm Ernst & Sohn, 2017. http://dx.doi.org/10.1002/9783433606667.

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10

Batoz, Jean-Louis. Geometrically nonlinear analysis of shell structures using flat DKT shell elements. Monterey, Calif: Naval Postgraduate School, 1985.

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11

Vaughan, R. E. An inelastic analysis of a welded aluminum joint. MSFC, Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 1994.

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12

Swansson, N. S. Application of finite element methods with cyclic elasto-plastic strain analysis to low cycle fatigue analysis of engine components (U). Melbourne, Australia: Aeronautical Research Laboratories, 1986.

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13

Dowling, Norman E. J-integral estimates for cracks in infinite bodies. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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14

Naik, Rajiv A. Failure analysis of woven and braided fabric reinforced composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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15

Naik, Rajiv A. Failure analysis of woven and braided fabric reinforced composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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16

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

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17

Gambrell, S. C. Use of photostress to analyze behavior of an aft skirt test specimen. Tuscaloosa, Ala: The University of Alabama, College of Engineering, Bureau of Engineering Research, 1994.

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18

International Conference on Computational Methods and Experimental Measurements (4th 1989 Capri, Italy). Computers and experiments in stress analysis: Proceedings of the fourth International Conference on Computational Methods and Experimental Measurements, Capri, Italy, May 1989. Edited by Carlomagno G. M, Brebbia C. A, International Society for Computational Methods in Engineering., and Computational Mechanics Institute (Southampton, England). Southampton: Computational Mechanics, 1989.

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19

Verderaime, V. Plate and butt-weld stresses beyond elastic limit, material and structural modeling. Marshall Space Flight Center, Ala: George C. Marshall Space Flight Center, 1991.

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20

Schindler, Paul. Optical fiber sensors for damage analysis in aerospace materials: Final report. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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21

Andrade, Maria João, and Albert Varga. Stress echocardiography: methodology. Oxford University Press, 2016. http://dx.doi.org/10.1093/med/9780198726012.003.0012.

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Stress echocardiography is the combination of echocardiography with a physical, pharmacological, or electrical stress. Good quality images are absolutely necessary and a quad-screen format should be applied for comparative analysis. Different stress echo protocols can be used in different pathologies. Exercise echocardiography has the advantages of its wide availability, low cost, and versatility for the assessment of various cardiac conditions. The most usual pathologies are suspected or known ischaemic heart disease, mitral and aortic valve diseases, hypertrophic cardiomyopathy, and pulmonary hypertension. Among exercise-independent stresses, dobutamine and dipyridamole are the most frequently used. Dobutamine is widely accepted for the evaluation of myocardial viability. The two tests have comparable accuracy for the detection of coronary artery disease. Ergonovine echo is highly feasible, accurate, and safe for the diagnosis of coronary vasospasm. High-rate pacing is especially appropriate in patients with a permanent pacemaker because non-invasive diagnosis of coronary artery disease in these patients is an extremely difficult task.
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22

Wang, Xinwei, and Akhtar S. Khan. Strain Measurements and Stress Analysis. Prentice Hall, 2000.

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23

Strain Measurements and Stress Analysis. Prentice Hall, 2000.

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24

Dally, James W. Experimental Stress Analysis. College House Enterprises Llc, 2001.

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25

Experimental Stress Analysis. College House Enterprises, 2005.

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26

1947-, Shchepinov V. P., ed. Strain and stress analysis by holographic and speckle interferometry. Chichester: J. Wiley, 1996.

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27

Pilkey, Walter D. Formulas for Stress, Strain, and Structural Matrices. Wiley & Sons, Incorporated, John, 2008.

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28

Pilkey, Walter D. Formulas for Stress, Strain, and Structural Matrices. Wiley, 2004.

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29

(Editor), G. M. Carlomagno, and C. A. Brebbia (Editor), eds. Computers and Experiments in Stress Analysis. WIT Press, 1989.

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30

Test load verification through strain data analysis. MSFC, Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 1995.

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31

Two-dimensional sequential and concurrent finite element analysis of unstiffened and stiffened aluminum and composite panels with hole. Norfolk, Va: Department of Civil Engineering, College of Engineering and Technology, Old Dominion University, 1988.

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32

Venkatesh, Prasad, and United States. National Aeronautics and Space Administration., eds. Two-dimensional sequential and concurrent finite element analysis of unstiffened and stiffened aluminum and composite panels with hole. Norfolk, Va: Department of Civil Engineering, College of Engineering and Technology, Old Dominion University, 1988.

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33

Schwitter, Juerg. Coronary artery disease. Edited by Dudley Pennell. Oxford University Press, 2018. http://dx.doi.org/10.1093/med/9780198784906.003.0105.

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In the work-up of suspected or known coronary artery disease (CAD), cardiovascular magnetic resonance (CMR) is an established technique and it is recommended by most recent guidelines. Stress dobutamine and stress perfusion CMR yield sensitivities and specificities to detect anatomically defined CAD (>50% coronary stenoses) ranging from 83% to 91% and from 83% to 86%, respectively, with areas under the receiver operating characteristic curve (AUCs) of 0.80–0.93. Multicentre trials report AUCs of 0.75–0.91 to detect CAD and showed superiority over scintigraphic techniques. Increasing evidence in thousands of patients demonstrates the highly predictive value of CMR. Exclusion of ischaemia by CMR goes along with excellent event-free survival rates of 0.5–0.9%/year. Cost analyses in large data sets (e.g. in the European CMR registry), suggest considerable cost savings for CMR over first-line invasive strategies in suspected CAD. Tissue characterization by CMR to detect scar, necrosis, oedema, microvascular obstruction, or haemorrhage is of particular importance in the setting of acute coronary syndromes and this application is emerging as the number of centres offering CMR increases.
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34

Keil, Stefan. Technology and Practical Use of Strain Gages: With Particular Consideration of Stress Analysis Using Strain Gages. Wiley & Sons, Limited, John, 2017.

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35

Technology and Practical Use of Strain Gages: With Particular Consideration of Stress Analysis Using Strain Gages. Wiley-VCH Verlag GmbH, 2017.

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36

Computer Aided Analysis of the Stress and Strain of Resp of High Polymer. CRC, 1993.

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37

Computer Aided Analysis of the Stress and Strain of Resp of High Polymer. CRC, 1993.

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38

Y, Hwang Shoi, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Local strain redistribution corrections for a simplified inelastic analysis procedure based on an elastic finite-element analysis. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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39

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

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40

M, Arnold S., and NASA Glenn Research Center, eds. An analysis of the macroscopic tensile behavior of a nonlinear nylon reinforced elastomeric composite system using MAC/GMC. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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41

An analysis of the macroscopic tensile behavior of a nonlinear nylon reinforced elastomeric composite system using MAC/GMC. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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42

M, Arnold Steven, and United States. National Aeronautics and Space Administration., eds. Driving force analysis in an infinite anisotropic plate with multiple crack interactions. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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43

United States. National Aeronautics and Space Administration., ed. J-integral estimates for cracks in infinite bodies. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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44

S, Raju I., O'Brien T. Kevin, Langley Research Center, and United States. Army Aviation Research and Technology Activity., eds. Strain energy release rate analysis of delamination in a tapered laminate subjected to tension load. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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45

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. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

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46

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. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

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47

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. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

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48

K, Binienda Wieslaw, Kreider K. L, and Lewis Research Center, eds. Analysis of multiple cracks in an infinite functionally graded plate. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.

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49

K, Binienda Wieslaw, Kreider K. L, and Lewis Research Center, eds. Analysis of multiple cracks in an infinite functionally graded plate. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.

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50

C, Stouffer Donald, and NASA Glenn Research Center, eds. Rate dependent deformation and strength analysis of polymer matrix composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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