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1

Tsourdalakis, Emmanuel. Phase transformations in TiA1 based alloy. Monterey, Calif: Naval Postgraduate School, 1991.

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2

Butt, M. Taqi Zahid. Study of gold-based alloy phase diagrams. Uxbridge: Brunel University, 1990.

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3

A, Nijs Johan F., ed. Advanced silicon and semiconducting silicon-alloy based materials and devices. Bristol: Institute of Physics Pub., 1994.

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4

Penton, Robert James Thomas. The fracture and fatigue of the Ti3Al based alloy super Alpha 2. Birmingham: University of Birmingham, 1994.

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5

W, Bransford J., and National Institute of Standards and Technology (U.S.), eds. Ignition characteristics of the nickel-based alloy UNS N07718 in pressurized oxygen. Boulder, Colo: U.S. Dept. of Commerce, National Institute of Standards and Technology, 1989.

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6

W, Bransford J., and National Institute of Standards and Technology (U.S.), eds. Ignition characteristics of the iron-based alloy UNS S66286 in pressurized oxygen. Boulder, Colo: U.S. Dept. of Commerce, National Bureau of Standards, 1988.

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7

Bransford, J. W. Ignition characteristics of the nickel-based alloy UNS N07001 in pressurized oxygen. Boulder, Colo: U.S. Dept. of Commerce, National Institute of Standards and Technology, 1990.

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8

Halford, Timothy Paul. Fatigue and fracture of a high strength, fully lamellar y-Tial based alloy. Birmingham: University of Birmingham, 2003.

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9

H, Titran Robert, and United States. National Aeronautics and Space Administration., eds. Tensile and stress-rupture behavior of hafnium carbide dispersed molybdenum and tungsten based alloy wires. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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10

H, Titran Robert, and United States. National Aeronautics and Space Administration., eds. Tensile and stress-rupture behavior of hafnium carbide dispersed molybdenum and tungsten based alloy wires. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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11

Center, Langley Research, ed. NASA-UVa light aerospace alloy and structure technology program supplement: Aluminum-based materials for high speed aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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12

Starke, E. A. NASA-UVa Light Aerospace Alloy and Structure Technology Program supplement: aluminum-based materials for high speed aircraft. Hampton, Va: Langley Research Center, 1993.

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13

Coelho, Reginaldo Teixeira. The machinability of aluminium-based SiC reinforced metal matrix composite (MMC) alloy with emphasis on hole production. Birmingham: University of Birmingham, 1995.

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14

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. NASA-UVa light aerospace alloy and structure technology program suppleyment: Aluminum-based materials for high speed aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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15

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. NASA-UVa light aerospace alloy and structure technology program supplement: Aluminum-based materials for high speed aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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16

A, Starke E., Langley Research Center, and University of Virginia. School of Engineering and Applied Science., eds. NASA-UVa Light Aerospace Alloy and Structures Technology Program: Aluminum-based materials for high speed aircraft : final report. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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17

Sheakley, Brian J. Effect of water depth on the underwater wet welding of ferritic steels using austenitic Ni-based alloy electrodes. Monterey, Calif: Naval Postgraduate School, 2000.

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18

A, Starke E., Langley Research Center, and University of Virginia. School of Engineering and Applied Science., eds. NASA-UVa Light Aerospace Alloy and Structures Technology Program: Aluminum-based materials for high speed aircraft : semi-annual report January 1, 1993-June 30, 1993. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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19

E, Schwarze Gene, Niefra J. M, and United States. National Aeronautics and Space Administration., eds. Comparison of high temperature, high frequency core loss and dynamic B-H loops of two 50 Ni-Fe crystalline alloys and an iron-based amorphous alloy. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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20

Center, Langley Research, ed. NASA-UVa light aerospace alloy and structures technology program supplement: Aluminum-based materials for high speed aircraft : semi-annual report July 1, 1992 - December 31, 1992. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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21

Starke, E. A. NASA-UVa light aerospace alloy and structures technology program supplement: aluminum-based materials for high speed aircraft: semi-annual report, July 1, 1992-December 31, 1992. Hampton, Va: Langley Research Center, 1995.

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22

Center, Langley Research, ed. NASA-UVa light aerospace alloy and structures technology program supplement: Aluminum-based materials for high speed aircraft : semi-annual report July 1, 1992 - December 31, 1992. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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23

Center, Langley Research, ed. NASA-UVa light aerospace alloy and structures technology program supplement: Aluminum-based materials for high speed aircraft : semi-annual report July 1, 1992 - December 31, 1992. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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24

A, Starke E., and Langley Research Center, eds. NASA-UVa Light Aerospace Alloy and Structures Technology Program: Aluminum-based materials for high speed aircraft : semi-annual report January 1, 1993-June 30, 1993, under grant NAG1-745. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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25

A, Starke E., and Langley Research Center, eds. NASA-UVa Light Aerospace Alloy and Structures Technology Program: Aluminum-based materials for high speed aircraft : semi-annual report January 1, 1993-June 30, 1993, under grant NAG1-745. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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26

A, Starke E., and Langley Research Center, eds. NASA-UVa Light Aerospace Alloy and Structures Technology Program: Aluminum-based materials for high speed aircraft : semi-annual report January 1, 1993-June 30, 1993, under grant NAG1-745. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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27

Ren, Binyan. The recrystallization of an Al-Li-Zr based alloy. 1988.

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28

Nijs, Johan F. A., ed. Advanced Silicon and Semiconducting Silicon-Alloy Based Materials and Devices. CRC Press, 2021. http://dx.doi.org/10.1201/9781003208860.

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29

Nijs, Jo. Advanced Silicon and Semiconducting Silicon-Alloy Based Materials and Devices. Taylor & Francis Group, 2021.

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30

Nijs, Jo. Advanced Silicon and Semiconducting Silicon-Alloy Based Materials and Devices. Taylor & Francis Group, 2021.

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31

Nijs, Jo. Advanced Silicon and Semiconducting Silicon-Alloy Based Materials and Devices. Taylor & Francis Group, 2021.

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32

Nijs, Jo. ADVANCED SILICON and SEMICONDUCTING SILICON-ALLOY BASED MATERIALS and DEVICES. Taylor & Francis Group, 2019.

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33

Morinaga, Masahiko. Quantum Approach to Alloy Design: An Exploration of Material Design and Development Based upon Alloy Design Theory and Atomization Energy Method. Elsevier, 2018.

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34

Morinaga, Masahiko. A Quantum Approach to Alloy Design: An Exploration of Material Design and Development Based Upon Alloy Design Theory and Atomization Energy Method. Elsevier, 2018.

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35

Tomashyk, Vasyl. Quaternary Alloys Based on II - VI Semiconductors. Taylor & Francis Group, 2014.

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36

Tomashyk, Vasyl. Quaternary Alloys Based on II - VI Semiconductors. Taylor & Francis Group, 2014.

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37

Tomashyk, Vasyl. Quaternary Alloys Based on II - VI Semiconductors. Taylor & Francis Group, 2014.

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38

Tomashyk, Vasyl. Quaternary Alloys Based on II - VI Semiconductors. Taylor & Francis Group, 2019.

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39

Tensile and stress-rupture behavior of hafnium carbide dispersed molybdenum and tungsten based alloy wires. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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40

Tensile and stress-rupture behavior of hafnium carbide dispersed molybdenum and tungsten based alloy wires. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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41

Grove-Rasmussen, K. Hybrid Superconducting Devices Based on Quantum Wires. Edited by A. V. Narlikar. Oxford University Press, 2017. http://dx.doi.org/10.1093/oxfordhb/9780198738169.013.16.

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This article reviews the experimental progress in hybrid superconducting devices based on quantum wires, in the form of semiconductor nanowires or carbon nanotubes, which are coupled to superconducting electrodes. It also presents a series of recent examples which illustrate the key phenomena that have allowed detailed investigations of important scenarios, including individual impurities on superconductors and proximitized systems that may hold Majorana quasiparticles. After describing experimental aspects of hybrid devices, including materials and fabrication techniques, the article considers superconducting junctions with normal quantum dots (QDs). It then turns to experiments on superconductivity-enhanced QD spectroscopy, sub-gap states in hybrid QDs, and non-local signals in Cooper pair splitter devices. Finally, it discusses the growth of epitaxial semiconductor–superconductor nanowire hybrids.
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42

NASA-UVa light aerospace alloy and structure technology program supplement: Aluminum-based materials for high speed aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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43

NASA-UVa light aerospace alloy and structure technology program supplement: Aluminum-based materials for high speed aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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44

NASA-UVa light aerospace alloy and structure technology program suppleyment: Aluminum-based materials for high speed aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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45

Siddiquee, Arshad Noor, Sandeep Rathee, Manu Srivastava, Sachin Maheshwari, and T. K. Kundra. Friction Based Additive Manufacturing Technologies. Taylor & Francis Group, 2021.

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46

Giessen, B. C. Developments in the Structural Chemistry of Alloy Phases: Based on a Symposium Sponsored by the Committee on Alloy Phases of the Institute of Metals Division, the Metallurgical Society, American Institute of Mining, Metallurgical and Petroleum Engineers, Cleveland, Ohio, October 1967. Springer, 2014.

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47

Giessen, B. C. Developments in the Structural Chemistry of Alloy Phases: Based on a Symposium Sponsored by the Committee on Alloy Phases of the Institute of Metals Division, the Metallurgical Society, American Institute of Mining, Metallurgical and Petroleum Engineers, Cleveland, Ohio, October 1967. Springer, 2013.

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48

Mann, Elizabeth C. L. An investigation into test frequency effects on the corrosion fatigue crack growth threshold of 7075-T6 aluminium-alloy using a personal computer based automated system. 1985.

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49

Friction Based Additive Manufacturing Technologies: Principles for Building in Solid State, Benefits, Limitations, and Applications. Taylor & Francis Group, 2018.

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50

Siddiquee, Arshad Noor, Sandeep Rathee, Manu Srivastava, Sachin Maheshwari, and T. K. Kundra. Friction Based Additive Manufacturing Technologies: Principles for Building in Solid State, Benefits, Limitations, and Applications. Taylor & Francis Group, 2018.

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