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Books on the topic 'Cooling flow'

Author: Grafiati

Published: 4 June 2021

Last updated: 1 February 2022

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1

Simon, Frederick F. Jet model for slot film cooling with effect of free-stream and coolant turbulence. Lewis Research Center, 1986.

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2

Garg, Vijay Kumar. Effect of coolant temperature and mass flow on film cooling of turbine blades. National Aeronautics and Space Administration, 1997.

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3

Mills, Anthony F. Fluid flow and heat convection studies for actively cooled airframes. National Aeronautics and Space Administration, 1993.

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4

Mills, Anthony F. Fluid flow and heat convection studies for actively cooled airframes. National Aeronautics and Space Administration, 1993.

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5

Benocci, C. A prediction method for the air-droplets flow in the inlet section of a natural draught cooling tower. von Karman Institute for Fluid Dynamics, 1986.

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6

Yamamoto, Atsumasa. Effects of cooling-air injection on secondary flows and losses in a turbine cascade. National Aerospace Laboratory, 1991.

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7

Kim, K. Assessment of RELAP5/MOD2 critical flow model using Marviken test data 15 and 24. Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1992.

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8

Kim, Kyu-Soo. Assessment of RELAP5/MOD2 critical flow model using Marviken test data 15 and 24. Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1992.

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9

Styrikovich, M. A. Two-phase cooling and corrosion in nuclear power plants. Edited by Polonskiĭ V. S, T͡S︡iklauri G. V, and Hewitt G. F. Hemisphere Pub. Corp., 1987.

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10

Mills, Anthony F. Fluid flow and heat convection studies for actively cooled airframes, May 1992 - October 1992. National Aeronautics and Space Administration, 1992.

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11

Mills, Anthony F. Fluid flow and heat convection studies for actively cooled airframes, May 1992 - October 1992. National Aeronautics and Space Administration, 1992.

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12

Heidmann, James D. Coarse grid modeling of turbine film cooling flows using volumetric source terms. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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13

Kousa, Maunu. Numerical and experimental modelling of gas flow and heat transfer in the air gap of an electric machine. Lappeenranta University of Technology, 2002.

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14

Canada, Atomic Energy of. Post-test simulations of BTF-107: An in-reactor loss-of-coolant test with flow blockage and rewet. Chalk River Laboratories, 1993.

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15

D, Butler. Development and integration of the Capillary Pumped Loop GAS and Hitchhiker flight experiments. National Aeronautics and Space Administration, Goddard Space Flight Center, 1990.

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16

Palatka, Robert M. Numerical analysis of the flow in a turbulated rectangular duct simulating the cooling passages in a turbine blade. Naval Postgraduate School, 1992.

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17

Foley, W. J. Closeout of IE bulletin 86-01: Minimun flow logic problems that could disable residual heat removal pumps. Division of Operational Events Assessment, Office of Nuclear Reactor Regulation, U.S. Nuclear Regulatory Commission, 1989.

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18

Lepicovsky, J. Application of thin-film thermocouples to localized heat transfer measurements. National Aeronautics and Space Administration, 1995.

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19

Lepicovsky, J. Application of thin-film thermocouples to localized heat transfer measurements. National Aeronautics and Space Administration, 1995.

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20

Rodriguez, Ferdinand. Principles of polymer systems. 3rd ed. Hemisphere Pub. Corp., 1989.

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21

Rodriguez, Ferdinand. Principles of polymer systems. 4th ed. Taylor & Francis, 1996.

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22

Rodriguez, Ferdinand. Principles of polymer systems. 4th ed. Taylor & Francis, 1996.

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23

Melʹnikov, V. I. Akusticheskie metody diagnostiki dvukhfaznykh teplonositeleĭ I͡A︡ĖU. Ėnergoatomizdat, 1987.

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24

Bejan, Adrian, and Giuseppe Grazzini, eds. Shape and Thermodynamics. Firenze University Press, 2008. http://dx.doi.org/10.36253/978-88-8453-836-9.

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Shape and Thermodynamics is a two-day international Workshop focused on the Constructal Theory of generation of configuration in nature and engineering. From the early developments related to tree configurations for the cooling of electronics, today Constructal theory is being applied to conceptual design of transportation net-works, river basins, living bodies, building materials and many other flow systems. Constructal theory is also enriching thermo-dynamics, from basic theory to design and optimization. This theory approaches design "as science", with the generation of configuration regard

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25

NATO, Advanced Research Workshop on Cooling Flows in Clusters and Galaxies (1987 Cambridge England). Cooling flows in clusters and galaxies. Kluwer Academic Publishers, 1988.

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26

Fabian, A. C., ed. Cooling Flows in Clusters and Galaxies. Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2953-1.

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27

Stone, James M. The stability of radiatively cooling jets. National Aeronautics and Space Administration, 1997.

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28

Solar technologies for buildings. Wiley, 2003.

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29

Eicker, Ursula. Solar Technologies for Buildings. John Wiley & Sons, Ltd., 2006.

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30

L, Haggard Kenneth, ed. Passive solar architecture: Heating, cooling, ventilation, daylighting and more using natural flows. Chelsea Green Pub., 2010.

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31

Nan-Suey, Liu, and NASA Glenn Research Center, eds. Film cooling flow effects on post-combustor trace chemistry. National Aeronautics and Space Administration, Glenn Research Center, 2003.

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32

J, Roelke Richard, Meitner Peter L, and United States. National Aeronautics and Space Administration., eds. A generalized one dimensional computer code for turbomachinery cooling passage flow calculations. National Aeronautics and Space Administration, 1989.

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33

Talbot, Michael T. Pressure and velocity distribution for air flow through fruits packed in shipping containers using porous media flow analysis. 1987.

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34

Sung-jin, Kim, and Lee Sang-Woo, eds. Air cooling technology for electronic equipment. CRC Press, 1996.

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35

1934-, Hoffman Joe D., and United States. National Aeronautics and Space Administration., eds. The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios. National Aeronautics and Space Administration, 1994.

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36

Center, Huntsville Engineering, and United States. National Aeronautics and Space Administration., eds. Fluid flow analysis of the SSME high pressure fuel and oxidizer turbine coolant systems. Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center, 1990.

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37

H, Wagner Joel, and United States. National Aeronautics and Space Administration., eds. Heat transfer experiments in the internal cooling passages of a cooled radial turbine rotor. National Aeronautics and Space Administration, 1996.

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38

H, Wagner Joel, and United States. National Aeronautics and Space Administration., eds. Heat transfer experiments in the internal cooling passages of a cooled radial turbine rotor. National Aeronautics and Space Administration, 1996.

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39

United States. National Aeronautics and Space Administration., ed. A numerical study of the effect of wake passing on turbine blade film cooling. National Aeronautics and Space Administration, 1995.

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40

Clarke, Andrew. Energy flow in organisms. Oxford University Press, 2017. http://dx.doi.org/10.1093/oso/9780199551668.003.0004.

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An organism is an open thermodynamic system exchanging both energy and materials with its environment. Organisms exchange energy with their environment by radiation, conduction, convection and evaporation of water. The relative importance of these varies with the organism and its situation. Newton’s Law of Cooling is a simplification that is useful only for warm endotherms in a still, cool environment. For all other circumstances a full biophysical treatment is necessary. Flows of chemical potential energy can be captured by a balanced energy budget. A full description of the energy balance of

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41

-N, Tse D. G., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. A combined experimental/computational study of flow in turbine blade cooling passage. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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42

N, Tse D. G., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. A combined experimental/computational study of flow in turbine blade cooling passage. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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43

Wang, Lilac Cuiling. Numerical modeling of three-dimensional polymer melt flow in a cooling extruder. 2006.

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44

1933-, Nayfeh Ali Hasan, Ragab Saad, and United States. National Aeronautics and Space Administration., eds. Effect of wall cooling on the stability of compressible subsonic flows over smooth humps and backward-facing steps. Dept. of Engineering Science and Mechanics, Virginia Polytechnic Institute and State University, 1989.

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45

J, Nowak Robert, and United States. National Aeronautics and Space Administration., eds. Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream. National Aeronautics and Space Administration, 1995.

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46

Prediction of film cooling on gas turbine airfoils. National Aeronautics and Space Administration, 1994.

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47

Kroger, Detlev G. Air-Cooled Heat Exchangers and Cooling Towers: Thermal-Flow Performance Evaluation and Design. Begell House Publishers, 1999.

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48

United States. National Aeronautics and Space Administration., ed. Flow in serpentine coolant passages with trip strips: Technical progress narrative report, reporting period September 1, 1995 to September 30, 1995. Scientific Research Associates, 1995.

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49

Colpo, Sarah E. Pressurizer surge line Counter Current Flow Limitation during AP600 Mode 5 Cold Shutdown. 1999.

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50

Harry, Johnson, Margasahayam Ravi, and United States. National Aeronautics and Space Administration., eds. Nonintrusive flow rate determination through space shuttle water coolant loop floodlight coldplate. National Aeronautics and Space Administration, John F. Kennedy Space Center, 1997.

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