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Auteur : Grafiati
Publié le 14 mars 2023

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1

Whitehouse, Adrian Paul. Heat transfer fluid in an industrial process refrigeration system. Birmingham : University of Birmingham, 1991.

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2

C, Civinskas Kestutis, United States. National Aeronautics and Space Administration. et U.S. Army Research Laboratory., dir. Two-dimensional Navier-Stokes heat transfer analysis for rough turbine blades system. [Washington, DC : National Aeronautics and Space Administration, 1991.

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3

Boyle, Robert J. Two-dimensional Navier-Stokes heat transfer analysis for rough turbine blades system. [Washington, DC : National Aeronautics and Space Administration, 1991.

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4

Boyle, Robert J. Two-dimensional Navier-Stokes heat transfer analysis for rough turbine blades system. [Washington, DC : National Aeronautics and Space Administration, 1991.

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5

Boyle, Robert J. Two-dimensional Navier-Stokes heat transfer analysis for rough turbine blades system. [Washington, DC : National Aeronautics and Space Administration, 1991.

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6

Clements, Joseph A. Heat transfer performance of a roof-spray cooling system employing the transfer function method. Springfield, Va : Available from the National Technical Information Service, 1993.

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7

Delil, A. A. M. Test loops for two-phase thermal management system components. Amsterdam, Netherlands : National Aerospace Laboratory, 1990.

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8

Heat transfer : Thermal management of electronics. Boca Raton : Taylor & Francis, 2010.

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9

Abdul-Aziz, Ali. Effects of cooling system parameters on heat transfer in PAFC stack. [Washington, DC : National Aeronautics and Space Administration, 1985.

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10

Heald, Edward E. Heat transfer : User guide for revision 5.1 : notes and exercises. Houston, PA (P.O. Box 65, Johnson Rd., Houston 15342-0065) : ANSYS, 1995.

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11

D, Quinn Robert, Gong Leslie et United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., dir. Finite-element reentry heat-transfer analysis of space shuttle orbiter. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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12

D, Quinn Robert, Gong Leslie et United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., dir. Finite-element reentry heat-transfer analysis of space shuttle orbiter. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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13

Ko, William L. Finite-element reentry heat-transfer analysis of space shuttle orbiter. Edwards, Calif : Dryden Flight Research Facility, 1986.

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14

United States. National Aeronautics and Space Administration., dir. The embodiment design of the heat rejection system for the portable life support system. [Washington, DC : National Aeronautics and Space Administration, 1994.

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15

Center, NAHB Research. Enerjoy case study : An evaluation of thermal comfort and energy consumption for the Energyjoy radiant panel heating system. Upper Marlboro, MD : NAHB Research Center, 1994.

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16

Centre, Bhabha Atomic Research, dir. Characterisation of girth pipe weld for primary heat transport system of pressurised heavy water reactors. Mumbai : Bhabha Atomic Research Centre, 2002.

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17

(Firm), VBB Allen. Feasibility of energy recovery for heat pump-assisted district heating & cooling from the Metro Renton wastewater treatment plant and effluent transfer system : Phase 2 report. Salem, Or : VBB Allen, 1986.

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18

S, Zakany James, et United States. National Aeronautics and Space Administration., dir. Metallized gelled propellants : Oxygen/RP-1/aluminum rocket heat transfer and combustion measurements. [Washington, D.C : National Aeronautics and Space Administration, 1996.

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19

Peck, Lindamae. Heat transfer and frost-thaw penetration in soil surrounding an inclusion of sand : Numerical model results relevant to electromagnetic sensor system performance. [Hanover, N.H] : US Army Corps of Engineers, Cold Regions Research & Engineering Laboratory, 1995.

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20

Peck, Lindamae. Heat transfer and frost-thaw penetration in soil surrounding an inclusion of sand : Numerical model results relevant to electromagnetic sensor system performance. [Hanover, N.H] : US Army Corps of Engineers, Cold Regions Research & Engineering Laboratory, 1995.

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21

Peck, Lindamae. Heat transfer and frost-thaw penetration in soil surrounding an inclusion of sand : Numerical model results relevant to electromagnetic sensor system performance. [Hanover, N.H] : US Army Corps of Engineers, Cold Regions Research & Engineering Laboratory, 1995.

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22

United States. National Aeronautics and Space Administration., dir. Effects of the cooling system parameters on heat transfer and performance of the PAFC stack during transient operation. [Cleveland, Ohio] : Cleveland State University, 1992.

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23

United States. National Aeronautics and Space Administration., dir. Effects of the cooling system parameters on heat transfer and performance of the PAFC stack during transient operation. [Cleveland, Ohio] : Cleveland State University, 1992.

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24

Delil, A. A. M. Sensors for a system to control the liquid flow into an evaporative cold plate of a two-phase heat transport system for large spacecraft. Amsterdam : National Aerospace Laboratory, 1986.

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25

S, Zakany James, et United States. National Aeronautics and Space Administration., dir. Metallized gelled propellants : Oxygen/RP-1/aluminum rocket heat transfer and combustion measurements. [Washington, D.C : National Aeronautics and Space Administration, 1996.

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26

United States. National Aeronautics and Space Administration., dir. Metallized gelled propellants : Oxygen/RP-1/aluminum rocket engine calorimeter heat transfer measurements and analysis. [Washington, D.C.] : National Aeronautics and Space Administration, 1997.

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27

Cavanagh, James Edward. Development of a high resolution, high heat transfer coolant system for the process control of cold strip rolling mills. Poole : Dorset Institute of Higher Education and Davy McKee (Poole) Ltd, 1985.

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28

N, Assanis Dennis, United States. Dept. of Energy. Office of Vehicle and Engine Research and Development. et United States. National Aeronautics and Space Administration., dir. A Computer simulation of the turbocharged turbocompounded Diesel engine system : A description of the thermodynamic and heat transfer models. Washington, D.C : U.S. Dept. of Energy, Conservation and Renewable Energy, Office of Vehicle and Engine R&D, 1986.

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29

H, Knoll Richard, et United States. National Aeronautics and Space Administration., dir. Thermal performance of a liquid hydrogen tank multilayer insulation system at warm boundary temperatures of 630, 530 and 152⁰ R. [Washington, D.C.] : National Aeronautics and Space Administration, 1991.

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30

Kveton, O. K. ITER cooling system : Analysis of heat transfer media, operation and safety of cooling loop and blanket during conditioning and baking. Toronto : Ontario Hydro, 1990.

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31

United States. National Aeronautics and Space Administration., dir. Metallized gelled propellants : Oxygen/RP-1/aluminum rocket engine calorimeter heat transfer measurements and analysis. [Washington, D.C.] : National Aeronautics and Space Administration, 1997.

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32

S, Zakany James, et United States. National Aeronautics and Space Administration., dir. Metallized gelled propellants : Oxygen/RP-1/aluminum rocket combustion experiments. [Washington, D.C.] : National Aeronautics and Space Administration, 1995.

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33

C, Ku Jerry, et United States. National Aeronautics and Space Administration., dir. Brief communication : Soot volume fraction maps for normal and reduced gravity laminar acetylene jet diffusion flames. [Washington, DC : National Aeronautics and Space Administration, 1997.

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34

C, Ku Jerry, et United States. National Aeronautics and Space Administration., dir. Brief communication : Soot volume fraction maps for normal and reduced gravity laminar acetylene jet diffusion flames. [Washington, DC : National Aeronautics and Space Administration, 1997.

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35

C, Ku Jerry, et United States. National Aeronautics and Space Administration., dir. Brief communication : Buoyancy-induced differences in soot morphology. [Washington, DC : National Aeronautics and Space Administration, 1995.

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36

Sigidov, Yuriy, Elena Kalashnikova et Tat'yana Horol'skaya. Primary accounting documentation. ru : INFRA-M Academic Publishing LLC., 2021. http://dx.doi.org/10.12737/1077324.

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The textbook sets out the theoretical foundations of the document flow of an economic entity, considers the stages of the movement of accounting documents from the moment of their creation to their transfer to storage, presents the procedure for registration of primary accounting documents on the facts of economic life in various parts of the accounting process in accordance with the requirements of Russian accounting and tax legislation. Meets the requirements of the federal state educational standards of higher education of the latest generation. It is intended for students in the field of training 38.03.01 "Economics", practicing accountants, economists, students of the advanced training system.
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37

S, Zakany James, et United States. National Aeronautics and Space Administration., dir. Metallized gelled propellants : Oxygen/RP-1/aluminum rocket combustion experiments. [Washington, D.C.] : National Aeronautics and Space Administration, 1995.

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38

Gilberto Francisco Martha de Souza. Thermal Power Plant Performance Analysis. London : Springer London, 2012.

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39

Desideri, Umberto, Giampaolo Manfrida et Enrico Sciubba, dir. ECOS 2012. Florence : Firenze University Press, 2012. http://dx.doi.org/10.36253/978-88-6655-322-9.

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The 8-volume set contains the Proceedings of the 25th ECOS 2012 International Conference, Perugia, Italy, June 26th to June 29th, 2012. ECOS is an acronym for Efficiency, Cost, Optimization and Simulation (of energy conversion systems and processes), summarizing the topics covered in ECOS: Thermodynamics, Heat and Mass Transfer, Exergy and Second Law Analysis, Process Integration and Heat Exchanger Networks, Fluid Dynamics and Power Plant Components, Fuel Cells, Simulation of Energy Conversion Systems, Renewable Energies, Thermo-Economic Analysis and Optimisation, Combustion, Chemical Reactors, Carbon Capture and Sequestration, Building/Urban/Complex Energy Systems, Water Desalination and Use of Water Resources, Energy Systems- Environmental and Sustainability Issues, System Operation/ Control/Diagnosis and Prognosis, Industrial Ecology.
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40

Heat transfer : User guide for revision 5.0. Houston, PA : Swanson Analysis Systems, 1993.

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41

Shabany, Younes. Heat Transfer : Thermal Management of Electronics. Taylor & Francis Group, 2009.

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42

Shabany, Younes. Heat Transfer : Thermal Management of Electronics. Taylor & Francis Group, 2009.

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43

Finite-element reentry heat-transfer analysis of space shuttle orbiter. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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44

Internal thermal control system hose heat transfer fluid thermal expansion evaluation test report. Marshall Space Flight Center, Ala : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 2001.

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45

Rezk, A. M. A. Heat and Fluid Flow in Power System Components : Hmt the Science and Applications of Heat and Mass Transfer. Elsevier Science & Technology Books, 2013.

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46

Finney, Mark, Sara McAllister, Torben Grumstrup et Jason Forthofer. Wildland Fire Behaviour. CSIRO Publishing, 2021. http://dx.doi.org/10.1071/9781486309092.

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Wildland fires have an irreplaceable role in sustaining many of our forests, shrublands and grasslands. They can be used as controlled burns or occur as free-burning wildfires, and can sometimes be dangerous and destructive to fauna, human communities and natural resources. Through scientific understanding of their behaviour, we can develop the tools to reliably use and manage fires across landscapes in ways that are compatible with the constraints of modern society while benefiting the ecosystems. The science of wildland fire is incomplete, however. Even the simplest fire behaviours – how fast they spread, how long they burn and how large they get – arise from a dynamical system of physical processes interacting in unexplored ways with heterogeneous biological, ecological and meteorological factors across many scales of time and space. The physics of heat transfer, combustion and ignition, for example, operate in all fires at millimetre and millisecond scales but wildfires can become conflagrations that burn for months and exceed millions of hectares. Wildland Fire Behaviour: Dynamics, Principles and Processes examines what is known and unknown about wildfire behaviours. The authors introduce fire as a dynamical system along with traditional steady-state concepts. They then break down the system into its primary physical components, describe how they depend upon environmental factors, and explore system dynamics by constructing and exercising a nonlinear model. The limits of modelling and knowledge are discussed throughout but emphasised by review of large fire behaviours. Advancing knowledge of fire behaviours will require a multidisciplinary approach and rely on quality measurements from experimental research, as covered in the final chapters.
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47

Design and test of a compact optics system for the pool boiling experiment. [Washington, D.C.] : NASA, 1990.

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48

X-34 experimental aeroheating at Mach 6 and 10. Reston, VA : American Institute of Aeronautics and Astronautics, 1998.

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49

Analysis of advanced solid rocket motor ignition phenomena : Final report. [Washington, DC : National Aeronautics and Space Administration, 1995.

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50

Gilberto Francisco Martha de Souza. Thermal Power Plant Performance Analysis. Springer, 2014.

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