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1

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. National Aeronautics and Space Administration, Glenn Research Center, 2003.

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2

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. National Aeronautics and Space Administration, Glenn Research Center, 2003.

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3

J, Larson H., and United States. National Aeronautics and Space Administration., eds. Development of advanced high temperature in-cylinder components and tribological systems for low heat rejection diesel engines: Phase 1, final report. National Aeronautics and Space Administration, 1992.

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4

Coccia, Gianluca, Giovanni Di Nicola, and Alejandro Hidalgo. Parabolic Trough Collector Prototypes for Low-Temperature Process Heat. Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-27084-5.

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5

Toal, Bernard Robert Hugh. The application of heat pumps to low temperature drying. The Author], 1985.

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6

Rhodes, RB, ed. Low Temperature Lubricant Rheology Measurement and Relevance to Engine Operation. ASTM International, 1992. http://dx.doi.org/10.1520/stp1143-eb.

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7

B, Rhodes Robert, ed. Low temperature lubricant rheology measurement and relevance to engine operation. ASTM, 1992.

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8

1948-, Bejan Adrian, Adorjan Alexander S, American Society of Mechanical Engineers. Heat Transfer Division., and National Heat Transfer Conference (28th : 1991 : Minneapolis, Minn.), eds. Cryogenic heat transfer, 1991. American Society of Mechanical Engineers, 1991.

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9

J, Boyle Robert, and NASA Glenn Research Center, eds. Infrared low temperature turbine vane rough surface heat transfer measurements. National Aeronautics and Space Administration, Glenn Research Center, 2000.

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10

O'Rourke, Gareth. The cryogenic heat treatment of tool steels. University College Dublin, 1998.

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11

Verkin, B. I. Teploobmen pri kipenii kriogennykh zhidkosteĭ. Nauk. dumka, 1987.

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12

Yen, Yin-Chao. Sensible heat flux measurements near a cold surface. U.S. Army Corps of Engineers, Cold Regions Research & Engineering Laboratory, 1995.

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13

Meeting, Materials Research Society. High temperature radiator materials for applications in the low earth orbital environment. [National Aeronautics and Space Administration], Lewis Research Center, 1987.

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14

E, Melis Matthew, and United States. National Aeronautics and Space Administration., eds. Hypersonic engine leading edge experiments in a high heat flux, supersonic flow environment. National Aeronautics and Space Administration, 1994.

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15

Yen, Yin-Chao. On the temperature distribution near a cold surface. U.S. Army Corps of Engineers, Cold Regions Research and Engineering Laboratory, 1993.

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16

Yen, Yin-Chao. On the temperature distribution near a cold surface. U.S. Army Corps of Engineers, Cold Regions Research & Engineering Laboratory, 1993.

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17

Marini͡uk, B. T. Vakuumno-isparitelʹnye kholodilʹnye ustanovki, teploobmenniki i gazifikatory tekhniki nizkikh temperatur. Ėnergoatomizdat, 2003.

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18

A, Kirichenko I͡U︡, and Fizyko-tekhnichnyĭ instytut nizʹkykh temperatur (Akademii͡a︡ nauk Ukraïnsʹkoï RSR), eds. Teplovye prot͡s︡essy v kriogennykh sistemakh: Sbornik nauchnykh trudov. Nauk. dumka, 1986.

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19

Matthias, Gottmann, and United States. National Aeronautics and Space Administration., eds. Thermal control systems for low-temperature heat rejection on a lunar base: Semiannual status report for grant NAG5-1572. Dept. of Aerospace and Mechanical Engineering, University of Arizona, 1992.

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20

Matthias, Gottmann, Nanjundan Ashok, and Goddard Space Flight Center, eds. Thermal control systems for low-temperature heat rejection on a lunar base: Annual progress report for grant NAG5-1572 (MOD). Aerospace and Mechanical Engineering, University of Arizona, 1993.

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21

Matthias, Gottmann, Nanjundan Ashok, and Goddard Space Flight Center, eds. Thermal control systems for low-temperature heat rejection on a lunar base: Annual progress report for grant NAG5-1572 (MOD). Aerospace and Mechanical Engineering, University of Arizona, 1993.

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22

J, Bougard, Afgan Naim, and International Center for Heat and Mass Transfer., eds. Heat and mass transfer in refrigeration and cryogenics. Hemisphere Pub. Corp., 1987.

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23

M, Kaviany, American Society of Mechanical Engineers. Heat Transfer Division., and AIAA/ASME Thermophysics and Heat Transfer Conference (6th : 1994 : Colorado Springs, Colo.), eds. Thermal phenomena at molecular and microscales and in cryogenic infrared detectors: Presented at the 6th AIAA/ASME Thermophysics and Heat Transfer Conference, Colorado Springs, Colorado, June 20-23, 1994. American Society of Mechanical Engineers, 1994.

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24

Chorowski, Maciej. Modelowanie termohydrauliki dekondukcji w magnesach nadprzewodzących. Oficyna Wydawnicza Politechniki Wrocławskiej, 2000.

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25

Liebert, Curt H. Heat flux measurement in SSME turbine blade tester. National Aeronautics and Space Administration, 1990.

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26

Gayda, John. High temperature fatigue crack growth behavior of Alloy 10. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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27

International, Mechanical Engineering Congress and Exposition (2004 Anaheim Calif ). Proceedings of the ASME Process Industries Division--2004: Presented at 2004 ASME Mechanical Engineering Congress and Exposition : November 13-19, 2004, Anaheim, California, USA. ASME, 2004.

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28

A, Papar Riyaz, American Society of Mechanical Engineers. Process Industries Division., American Society of Mechanical Engineers. Heat Transfer Division., American Society of Mechanical Engineers. Advanced Energy Systems Division., and International Mechanical Engineering Congress and Exposition (2001 : New York, N.Y.), eds. Proceedings of the ASME Process Industries Division, 2001 : presented at the 2001 ASME Mechanical Engineering Congress and Exposition, November 11-16, 2001, New York, New York. American Society of Mechanical Engineers, 2001.

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29

American Society of Mechanical Engineers. Process Industries Division. and International Mechanical Engineering Congress and Exposition (2005 : Orlando, Fla.), eds. Proceedings of the ASME Process Industries Division--2005 : presented at 2005 ASME Mechanical Engineering Congress and Exposition, November 5-11, 2005, Orlando, Florida, USA. ASME, 2005.

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30

N, Amineni, American Society of Mechanical Engineers. Process Industries Division., and International Mechanical Engineering Congress and Exposition (2003 : Washington, D.C.), eds. Proceedings of the ASME Process Industries Division--2003: Presented at the 2003 ASME Mechanical Engineering Congress : November 15-21, 2003, Washington, D.C. American Society of Mechanical Engineers, 2003.

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31

D, Craven P., Richards P. G, and United States. National Aeronautics and Space Administration., eds. A modified thermal conductivity for low density plasma magnetic flux tubes. American Geophysical Union, 1995.

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32

D, Craven P., Richards P. G, and United States. National Aeronautics and Space Administration., eds. A modified thermal conductivity for low density plasma magnetic flux tubes. American Geophysical Union, 1995.

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33

American Society of Mechanical Engineers. Process Industries Division. and International Mechanical Engineering Congress and Exposition (2006 : Chicago, Ill.), eds. Proceedings of the ASME Process Industries Division--2006 : presented at 2006 ASME International Mechanical Engineering Congress and Exposition, November 5-10, 2006, Chicago, Illinois, USA. American Society of Mechanical Engineers, 2007.

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34

United States. National Aeronautics and Space Administration., ed. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket engine calorimeter heat transfer measurements and analysis. National Aeronautics and Space Administration, 1997.

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35

Angelino, G. Design, construction and testing of a hermetically sealed 100 kw Organic Rankine Cycle engine formedium temperature (200-400°c) heat recovery. Commission of the European Communities, 1986.

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36

E, Nakori͡akov V., та Institut teplofiziki (Akademii͡a nauk SSSR), ред. Aktualʹnye voprosy teplofiziki i fizicheskoĭ gidrogazodinamiki: III Vsesoi͡uznai͡a konferent͡sii͡a molodykh issledovateleĭ, 28-30 marta 1989 g. Akademii͡a nauk SSSR, Sibirskoe otd-nie, In-t teplofiziki, 1989.

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37

United States. National Aeronautics and Space Administration., ed. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket engine calorimeter heat transfer measurements and analysis. National Aeronautics and Space Administration, 1997.

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38

United States. National Aeronautics and Space Administration., ed. Nickel-hydrogen battery state of charge during low rate trickle charging. National Aeronautics and Space Administration, 1995.

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39

United States. National Aeronautics and Space Administration., ed. Nickel-hydrogen battery state of charge during low rate trickle charging. National Aeronautics and Space Administration, 1995.

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40

Pavese, Franco. Modern Gas-Based Temperature and Pressure Measurements. 2nd ed. Springer US, 2013.

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41

W, Simon T., Oktay S, American Society of Mechanical Engineers. Heat Transfer Division., American Society of Mechanical Engineers. K-16 Committee on Heat Transfer in Electronic Equipment., and AIAA/ASME Thermophysics and Heat Transfer Conference (5th : 1990 : Seattle, Wash.), eds. Cryogenic and immersion cooling of optics and electronic equipment: Presented at AIAA/ASME Thermophysics and Heat Transfer Conference, June 18-20, 1990, Seattle, Washington. American Society of Mechanical Engineers, 1990.

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42

Stephan, K. Thermal conductivity and viscosity data of fluid mixtures. Dechema, 1988.

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43

United States. National Aeronautics and Space Administration., ed. Investigation of heat transfer in zirconium potassium percholate at low temperature: A study of the failure mechanism of the NASA standard initiator : final technical report for the period August 1, 1988-August 31, 1989. University of Texas at Austin, Center for Energy Studies, 1989.

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44

Meeting, American Society of Mechanical Engineers Winter. Low temperature biotechnology: Emerging applications and engineering contributions : presented at the Winter Annual Meeting of the American Society of Mechanical Engineers, Chicago, Illinois, November 27-December 2, 1988 ; sponsored by the Bioengineering Division and the Heat Division, ASME ; edited by J.J. McGrath, K.R. Diller. The American Society of Mechanical Engineers, 1988.

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45

J, Marchand, Pigeon Michel, Setzer M, and International Workshop on Freeze-Thaw and De-icing Resistance of Concrete (Lund, Sweden), eds. Freeze-thaw durability of concrete: Proceedings of the International Workshop in the Resistance of Concrete to Scaling Due to Freezing in the Prsence of De-icing Salts, Sainte-Foy, Québec, Canada : papers from the International Workshop on Freeze-Thaw and De-icing Resistance of Concrete, Lund, Sweden. E & FN Spon, 1997.

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46

Nechaev, Vladimir, Andrey Shuba, Stanislav Gridnev, and Vitaliy Topolov. Dimensional effects in phase transitions and physical properties of ferroics. INFRA-M Academic Publishing LLC., 2022. http://dx.doi.org/10.12737/1898400.

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The monograph presents mathematical methods and a set of mathematical models describing, within the framework of phenomenological theory, phase transitions in 0D-. 1D-, 2D-, 3D-dimensional ferroelectrics, ferroelastics, ferromagnets and their static and dynamic physical properties near the phase transition point. The influence of the parameters characterizing the ferroic sample and its interaction with the environment on the features of the phase transition, phase transition temperature shift, heat capacity, generalized susceptibilities is analyzed. Mathematical models of multilayer thin-film
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47

Sherwood, Dennis, and Paul Dalby. Temperature and heat. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198782957.003.0003.

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Concepts of temperature, temperature scales and temperature measurement. The ideal gas law, Dalton’s law of partial pressure. Assumptions underlying the ideal gas, and distinction between ideal and real gases. Introduction to equations-of-state such as the van der Waals, Dieterici, Berthelot and virial equations, which describe real gases. Concept of heat, and distinction between heat and temperature. Experiments of Rumford and Joule, and the principle of the conservation of energy. Units of measurement for heat. Heat as a path function. Flow of heat down a temperature gradient as an irreversi
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48

Modeling of high-strain-rate deformation, fracture, and impact behavior of advanced gas turbine engine materials at low and elevated temperatures. National Aeronautics and Space Administration, Glenn Research Center, 2003.

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49

Development of high temperature liquid lubricants for low-heat rejection heavy duty diesel engines. National Aeronautics and Space Administration, Lewis Research Center, 1993.

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50

Development of advanced high temperature in-cylinder components and tribological systems for low heat rejection diesel engines: Phase 1, final report. National Aeronautics and Space Administration, 1992.

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