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1

G, Ifju Peter, and Langley Research Center, eds. Through-the-thickness tensile strength of textile composites. National Aeronautics and Space Administration, Langley Research Center, 1994.

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2

G, Ifju Peter, and Langley Research Center, eds. Through-the-thickness tensile strength of textile composites. National Aeronautics and Space Administration, Langley Research Center, 1994.

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3

C, Newman J., Grandt A. F. 1945-, and Langley Research Center, eds. Through-the-thickness fatigue crack closure behavior in an aluminum alloy. National Aeronautics and Space Administration, Langley Research Center, 1990.

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4

C, Newman J., Grandt A. F. 1945-, and Langley Research Center, eds. Through-the-thickness fatigue crack closure behavior in an aluminum alloy. National Aeronautics and Space Administration, Langley Research Center, 1990.

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5

Horban, Blaise A. The effects of through the thickness delaminations on curved composite panels. Air Force Institute of Technology, Dept. of the Air Force, Air University, 1985.

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6

Dawicke, D. S. Through-the-thickness fatigue crack closure behavior in an aluminum alloy. National Aeronautics and Space Administration, Langley Research Center, 1990.

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7

United States. National Aeronautics and Space Administration., ed. Post-impact fatigue of cross-plied, through-the-thickness reinforced carbon/expoxy composites. National Aeronautics and Space Administration, 1994.

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8

United States. National Aeronautics and Space Administration., ed. Post-impact fatigue of cross-plied, through-the-thickness reinforced carbon/expoxy composites. National Aeronautics and Space Administration, 1994.

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9

United States. National Aeronautics and Space Administration., ed. Post-impact fatigue of cross-plied, through-the-thickness reinforced carbon/expoxy composites. National Aeronautics and Space Administration, 1994.

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10

United States. National Aeronautics and Space Administration., ed. Post-impact fatigue of cross-plied, through-the-thickness reinforced carbon/expoxy composites. National Aeronautics and Space Administration, 1994.

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11

V, Sankar Bhavani, and United States. National Aeronautics and Space Administration., eds. Effects of through-the-thickness stitching on impact and interlaminar fracture properties of textile graphite/epoxy laminates. National Aeronautics and Space Administration, Langley Research Center, 1995.

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12

V, Sankar Bhavani, and United States. National Aeronautics and Space Administration., eds. Effects of through-the-thickness stitching on impact and interlaminar fracture properties of textile graphite/epoxy laminates. National Aeronautics and Space Administration, Langley Research Center, 1995.

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13

Jacob, Aboudi, and Lewis Research Center, eds. HOTCFGM-1D: A coupled higher-order theory for cylindrical structural components with through-thickness functionally graded microstructures. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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14

Jacob, Aboudi, and Lewis Research Center, eds. HOTCFGM-1D: A coupled higher-order theory for cylindrical structural components with through-thickness functionally graded microstructures. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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15

Jacob, Aboudi, and Lewis Research Center, eds. HOTCFGM-1D: A coupled higher-order theory for cylindrical structural components with through-thickness functionally graded microstructures. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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16

V, Sankar Bhavani, and United States. National Aeronautics and Space Administration., eds. Effects of through-the-thickness stitching on impact and interlaminar fracture properties of textile graphite/epoxy laminates. National Aeronautics and Space Administration, Langley Research Center, 1995.

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17

Hyer, M. W. A simple evaluation of thermally-induced stresses in the vicinity of the stitch in a through-thickness reinforced cross-ply laminate. Center for Composite Materials and Structures, Virginia Tech, Virginia Polytechnic Institute and State University ; [Washington, DC, 1994.

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18

Nevalainen, Markku J. Fracture toughness comparison between a semielliptical surface crack in a 4PB plate and a through-thickness crack in a 3PB fracture toughness test specimen. VTT, Technical Research Centre of Finland, 1997.

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19

United States. National Aeronautics and Space Administration., ed. [Damage assessment and residual compression strength of thick composite plates with through-the-thickness reinforcements]: Semi-annual report for NASA grant NAG-1-1063, period: November 1, 1989 - June 1, 1990. National Aeronautics and Space Administration, 1990.

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20

Through-the-thickness tensile strength of textile composites. National Aeronautics and Space Administration, Langley Research Center, 1994.

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21

Through-the-thickness tensile strength of textile composites. National Aeronautics and Space Administration, Langley Research Center, 1994.

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22

Through-the-thickness fatigue crack closure behavior in an aluminum alloy. National Aeronautics and Space Administration, Langley Research Center, 1990.

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23

Ho-Chih Kuan Chuang-Tao Pak Chin. Numerical Method of 1000-Mb Prognosis Through Prediction of Thickness Field. Creative Media Partners, LLC, 2021.

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24

Kao, Hung. X-ray computerized tomography of particleboard to predict through-thickness density profile. 1990.

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25

Kao, Hung. X-ray computerized tomography of particleboard to predict through-thickness density profile. 1990.

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26

Allen, A. J., M. T. Hutchings, and V. Rainey. Measurement of Through-thickness Residual Stress in Offshore Steels Using the Neutron Diffraction Technique. AEA Technology Plc, 1986.

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27

HOTCFGM-1D: A coupled higher-order theory for cylindrical structural components with through-thickness functionally graded microstructures. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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28

National Aeronautics and Space Administration (NASA) Staff. Effects of Through-The-Thickness Stitching on Impact and Interlaminar Fracture Properties of Textile Graphite/Epoxy Laminates. Independently Published, 2018.

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29

Development and Implementation of a Shell Element With Pressure Variation Through the thickness and Void Growth and Nucleation Effects. Storming Media, 1999.

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30

Chance, Kelly, and Randall V. Martin. Radiative Transfer. Oxford University Press, 2017. http://dx.doi.org/10.1093/oso/9780199662104.003.0004.

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Radiative transfer is the process of energy transfer during the propagation of electromagnetic radiation through a medium. The processes of extinction, due to absorption and scattering, and thermal emission are described. It is shown how they can be represented by wavelength-dependent optical thickness, due to absorption or emission cross sections and the number of absorbers, emitters, or scatterers. Cloud optical thickness and conservative scattering are described. The scattering phase function is introduced. Next, the general form of radiative transfer is given, and its applicability to the
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31

Johnson, Ryan J. On the Surface: The Deleuze-Stoicism Encounter. Edinburgh University Press, 2018. http://dx.doi.org/10.3366/edinburgh/9781474412094.003.0015.

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Ryan J. Johnson’s “On the Surface: The Deleuze-Stoicism Encounter” investigates Deleuze’s reworking of Stoic ontology and the theory of incorporeals. Contrary to the traditional interpretation, Johnson argues that there are three, not four, primary incorporeals: space, λεκτόν‎, and time. Deploying Deleuze’s thinking of the intensive-extensive ontological distinction, Johnson shows that each of the three incorporeals are paradoxically structured by the slight Stoic surface-without-thickness separating and connecting their respective extensive and intensive dimensions (place/void, verb/noun, Aio
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32

Weld-Through Inorganic Zinc Primer. AMPP, 2004. https://doi.org/10.5006/sspc-paint_30-2004.

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Scope This specification covers a group of inorganic zinc primers that can protect carbon steel during the fabrication process, permit welding to specification requirements, and be overcoated. The major pigment component in this coating is zinc dust and the binder is inorganic. This specification defines the minimum compositional and laboratory performance requirements for characterizing a group of zinc primers. It is to be used in conjunction with SSPC-PS Guide 22.00, SSPC-PS Guide 12.00, and other SSPC specifications covering surface preparation, application, thickness, inspection, and safet
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33

Perry, Steven F., Markus Lambertz, and Anke Schmitz. Respiratory Biology of Animals. Oxford University Press, 2019. http://dx.doi.org/10.1093/oso/9780199238460.001.0001.

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The aim of this book is to shed light on one of the most fundamental processes of life in the various lineages of animals: respiration. It provides a certain background on the physiological side of respiration, but it clearly focuses on the morphological aspects. In general, the intention of this book is to illustrate the impressive diversity of respiratory faculties (form–function complexes) rather than serving as an encyclopaedic handbook. It takes the reader on a journey through the entire realm of animals and discusses the structures involved in gas exchange, how they work, and most import
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34

Keshav, Satish, and Alexandra Kent. Inflammatory bowel disease. Edited by Patrick Davey and David Sprigings. Oxford University Press, 2018. http://dx.doi.org/10.1093/med/9780199568741.003.0203.

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Inflammatory bowel disease (IBD) encompasses ulcerative colitis (UC) and Crohn’s disease (CD). Both conditions cause chronic relapsing inflammation in the gastrointestinal (GI) tract, but have different characteristics. UC causes diffuse mucosal inflammation limited to the colon, extending proximally from the anal verge, with the rectum involved in 95% of patients. UC is described in terms of the disease extent: proctitis (confined to the rectum), proctosigmoiditis (disease confined to the recto-sigmoid colon), distal disease (distal to the splenic flexure), and pan-colitis (the entire large i
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