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1

Birmingham), Autotech 1991 (1991. Engine cooling systems. Institution of Mechanical Engineers, 1991.

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2

Engineers, Society of Automotive, and SAE International Congress & Exposition (1996 : Detroit, Mich.), eds. Engine coolants and cooling system components. Society of Automotive Engineers, 1996.

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3

SAE International Congress & Exposition (1992 : Detroit, Mich.), ed. New engine design and cooling systems. Society of Automotive Engineers, 1992.

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4

Kanefsky, Peter. A systems approach to engine cooling design. Society of Automotive Engineers, 1999.

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5

Engineers, Society of Automotive, and SAE International Congress & Exposition (1993 : Detroit, Mich.), eds. Engine coolants, cooling system materials, and components. Society of Automotive Engineers, 1993.

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6

Society of Automotive Engineers. Transportation & Maintenance Technical Committee. and Society of Automotive Engineers. Cooling Systems Standards Committee., eds. Principles of engine cooling systems, components, and maintenance. 4th ed. Society of Automotive Engineers, 1991.

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7

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Thermal stratification potential in rocket engine coolant channels. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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8

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Thermal stratification potential in rocket engine coolant channels. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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9

Eaton, Edward R. Global testing of extended service engine coolants and related fluids. ASTM International, 2014.

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10

Kanda, Takeshi. Effect of regenerative cooling on rocket engine specific impulse. National Aerospace Laboratory, 1993.

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11

Kacynski, Kenneth J. Thermal stratification potential in rocket engine coolant channels. Lewis Research Center, 1992.

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12

Engineers, Society of Automotive, and SAE International Congress & Exposition (1990 : Detroit, Mich.), eds. Worldwide trends in engine collants, cooling system materials and testing. Society of Automotive Engineers, 1990.

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13

Armstrong, Elizabeth S. Cooling of rocket thrust chambers with liquid oxygen. NASA, 1990.

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14

Armstrong, Elizabeth S. Cooling of rocket thrust chambers with liquid oxygen. NASA, 1990.

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15

Engineers, Society of Automotive, and SAE International Congress and Exposition (1990 : Detroit, Mich.), eds. Worldwide trends in engine coolants, cooling system materials and testing. Society of Automotive Engineers, 1990.

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16

R, Conners Timothy, and Dryden Flight Research Facility, eds. Flight evaluation of an extended engine life mode on an F-15 airplane. National Aeronautics and Space Administration, Dryden Flight Research Facility, 1992.

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17

R, Conners Timothy, and Dryden Flight Research Facility, eds. Flight evaluation of an extended engine life mode on an F-15 airplane. National Aeronautics and Space Administration, Dryden Flight Research Facility, 1992.

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18

J, Gladden Herbert, and United States. National Aeronautics and Space Administration., eds. A unique high heat flux facility for testing hypersonic engine components. National Aeronautics and Space Administration, 1990.

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19

M, Kazaroff John, Jankovsky Robert S, and United States. National Aeronautics and Space Administration., eds. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis. National Aeronautics and Space Administration, 1991.

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20

M, Kazaroff John, Jankovsky Robert S, and United States. National Aeronautics and Space Administration., eds. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis. National Aeronautics and Space Administration, 1991.

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21

M, Kazaroff John, Jankovsky Robert S, and United States. National Aeronautics and Space Administration., eds. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis. National Aeronautics and Space Administration, 1991.

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22

F, Olfenbuttel Robert, Jones Jody A, and Risk Reduction Engineering Laboratory (U.S.), eds. Automotive and heavy-duty engine coolant recycling by distillation: Project summary. U.S. Environmental Protection Agency, Risk Reduction Engineering Laboratory, 1992.

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23

F, Olfenbuttel Robert, Jones Jody A, and Risk Reduction Engineering Laboratory (U.S.), eds. Automotive and heavy-duty engine coolant recycling by distillation: Project summary. U.S. Environmental Protection Agency, Risk Reduction Engineering Laboratory, 1992.

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24

F, Olfenbuttel Robert, Jones Jody A, and Risk Reduction Engineering Laboratory (U.S.), eds. Automotive and heavy-duty engine coolant recycling by distillation: Project summary. U.S. Environmental Protection Agency, Risk Reduction Engineering Laboratory, 1992.

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25

1962-, Gavaskar Arun R., and Risk Reduction Engineering Laboratory (U.S.), eds. Automotive and heavy-duty engine coolant recycling by filtration: Technology evaluation report. Risk Reduction Engineering Laboratory, Office of Research and Development, U.S. Environmental Protection Agency, c [1991], 1991.

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26

A, Lima Joseph, and Otterman George R, eds. Manual on selection and use of engine coolants and cooling system chemicals. 4th ed. ASTM, 1989.

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27

United States. National Aeronautics and Space Administration., ed. Electrically heated tube investigation of cooling channel geometry effects. National Aeronautics and Space Administration, 1995.

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28

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

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29

J, Bruckner R., Smith F. A, and United States. National Aeronautics and Space Administration., eds. Application of thin-film thermocouples to localized heat transfer measurements. National Aeronautics and Space Administration, 1995.

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30

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

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31

Center, Lewis Research, ed. The effect of cooling passage aspect ratio on curvature heat transfer enhancement. National Aeronautics and Space Administration, Lewis Research Center, 1997.

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32

Johnson, Richard P. A preliminary design and analysis of an advanced heat-rejection system for an extreme altitude advanced variable cycle diesel engine installed in high-altitude advanced research plaftorm. National Aeronautics and Space Administration, Dryden Flight Research Facility, 1992.

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33

A, Klann Gary, United States. National Aeronautics and Space Administration., and United States. Army Aviation Systems Command., eds. Contingency power for a small turboshaft engine by using water injection into turbine cooling air. National Aeronautics and Space Administration, 1992.

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34

United States. National Aeronautics and Space Administration., ed. Evaluation of thermal barrier and PS-200 self-lubricating coatings in an air-cooled rotary engine. National Aeronautics and Space Administration, 1995.

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35

Center, Lewis Research, and United States. Army Aviation Systems Command., eds. Computer code for predicting coolant flow and heat transfer in turbomachinery. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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36

Jett, Timothy Raymond. Evaluation of bearing configurations using the single bearing tester in liquid nitrogen. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1991.

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37

Jett, Timothy Raymond. Evaluation of bearing configurations using the single bearing tester in liquid nitrogen. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1991.

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38

Silverstein, Calvin C. Heat pipe cooling for scramjet engines. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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39

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, ed. Heat pipe cooling for scramjet engines. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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40

Beal, RE, ed. Engine Coolant Testing: Third Volume. ASTM International, 1993. http://dx.doi.org/10.1520/stp1192-eb.

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41

Beal, RE, ed. Engine Coolant Testing: Fourth Volume. ASTM International, 1999. http://dx.doi.org/10.1520/stp1335-eb.

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42

Matulewicz, William N., ed. Engine Coolant Technologies: 5th Volume. ASTM International, 2008. http://dx.doi.org/10.1520/stp1491-eb.

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43

Symposium, on Engine Coolant: Development Testing and Use (1991 Scottsdale Ariz ). Engine coolant testing, third volume. ASTM, 1993.

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44

Beal, RE, ed. Engine Coolant Testing: Second Symposium. ASTM International, 1986. http://dx.doi.org/10.1520/stp887-eb.

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45

International Symposium on Engine Coolants and Their Testing (1997 Scottscdale, AZ). Engine coolant testing : fourth volume. Edited by Beal Roy E and ASTM Committee D-15 on Engine Coolants. ASTM, 1999.

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46

Engineers, Society of Automotive, and International Off-Highway & Powerplant Congress & Exposition (1999 : Indianapolis, Ind.), eds. New diesel engines, components, and cooling systems. Society of Automotive Engineers, 1999.

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47

Rigby, David L. Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn. National Aeronautics and Space Administration, Lewis Research Center, 1999.

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48

Armstrong, Elizabeth S. Liquid oxygen cooling of hydrocarbon fueled rocket thrust chambers. National Aeronautics and Space Administration, 1989.

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49

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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50

J, Martin Carl, Lucas Stephen H, and Langley Research Center, eds. Active cooling design for scramjet engines using optimization methods. National Aeronautics and Space Administration, Langley Research Center, 1988.

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