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Libros sobre el tema "Gas Turbine Cooling System"

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Publicado: 10 de marzo de 2023

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1

Stewart, William E. Design guide: Combustion turbine inlet air cooling systems. Atlanta, Ga: American Society of Heating, Refrigerating and Air-Conditioning Engineers, 1999.

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2

Ghodke, Chaitanya D. Gas Turbine Blade Cooling. Warrendale, PA: SAE International, 2018. http://dx.doi.org/10.4271/0768095069.

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3

Ghodke, Chaitanya. Gas Turbine Blade Cooling. Warrendale, PA: SAE International, 2018. http://dx.doi.org/10.4271/pt-196.

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4

Sandīpa, Datta y Ekkad Srinath 1958-, eds. Gas turbine heat transfer and cooling technology. 2a ed. Boca Raton, FL: Taylor & Francis, 2012.

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5

1953-, Dutta Sandip y Ekkad Srinath 1958-, eds. Gas turbine heat transfer and cooling technology. New York: Taylor & Francis, 2000.

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6

Naval Education and Training Program Management Support Activity (U.S.), ed. Gas turbine system technician (electrical) 3 & 2. [Pensacola, Fla.]: The Activity, 1988.

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7

Gonser, Robert W. Gas turbine system technician (electrical) 3 & 2. [Pensacola, Fla.]: The Activity, 1988.

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8

Ahern, John J. Gas turbine system technician (mechanical) 3 & 2. [Pensacola, Fla.]: The Center, 1985.

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9

Al-Khusaibi, T. M. S. Gas turbine models for power system analysis. Manchester: UMIST, 1993.

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10

Ahern, John J. Gas turbine system technician (mechanical) 3 & 2. Pensacola, Fla: The Activity, 1987.

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11

Kuzirian, Robert. Gas turbine systems supervisor. [Pensacola, Fla.]: The Activity, 1994.

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12

Roy, Langton, ed. Gas turbine propulsion systems. Chichester, West Sussex: Wiley, 2011.

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13

Filion, Julie A. Evaluating Inco's pellet unit off gas cooling system. Sudbury, Ont: Laurentian University, School of Engineering, 1998.

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14

Schobeiri, Meinhard T. Gas Turbine Design, Components and System Design Integration. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-58378-5.

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15

Schobeiri, Meinhard T. Gas Turbine Design, Components and System Design Integration. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-23973-2.

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16

Puffenbarger, Marshall B. Gas turbine system technician 1 & C, volume 1. [Pensacola, Fla.]: The Activity, 1987.

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17

Puffenbarger, Marshall B. Gas turbine system technician 1 & C, volume 1. [Pensacola, Fla.]: The Activity, 1987.

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18

United States. National Aeronautics and Space Administration., ed. Automotive gas turbine power system-performance analysis code. [Washington, DC]: National Aeronautics and Space Administration, 1997.

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19

J, Follen Gregory, Putt Charles W y United States. National Aeronautics and Space Administration., eds. Gas turbine system simulation: An object-oriented approach. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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20

Gonser, Robert W. Gas turbine system technician (electrical) 1 & C, volume 2. [Pensacola, Fla.]: The Activity, 1987.

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21

Puffenbarger, Marshall B. Gas turbine system technician (mechanical) 1 & C, volume 2. [Pensacola, Fla.]: The Activity, 1987.

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22

Puffenbarger, Marshall B. Gas turbine system technician (mechanical) 1 & C, volume 2. [Pensacola, Fla.]: The Activity, 1987.

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23

Gonser, Robert W. Gas turbine system technician (electrical) 1 & C, volume 2. [Pensacola, Fla.]: The Activity, 1987.

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24

Curlett, Brian P. Object-oriented approach for gas turbine engine simulation. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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25

Curlett, Brian P. Object-oriented approach for gas turbine engine simulation. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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26

D, Metz Stephen. Survey of gas tubine control for application to marine gas turbine propulsion system control. Monterey, Calif: Naval Postgraduate School, 1989.

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27

Davitt, James A. A baseline expert control system for marine gas turbine compressor surge. Monterey, California: Naval Postgraduate School, 1989.

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28

Summers, Robert L. Integrated exhaust gas analysis system for aircraft turbine engine component testing. [Washington, D.C.?]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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29

Gorla, Rama S. R. Probabilistic analysis of solid oxide fuel cell based hybrid gas turbine system. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

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30

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

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31

Davitt, James A. An evaluation of the potential for expert system application to marine gas turbine control. Monterey, Calif: Naval Postgraduate School, 1988.

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32

United States. National Aeronautics and Space Administration., ed. General Aviation Propulsion (GAP) Program, Turbine Engine System Element: Performance report, non-proprietary research results : NASA cooperative agreement no. NCC3-514. [Washington, DC: National Aeronautics and Space Administration, 1997.

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33

Center, NASA Glenn Research, ed. Overview of high-fidelity modeling activities in the numerical propulsion system simulations (NPSS) project. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.

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34

Veres, Joseph P. Overview of high-fidelity modeling activities in the numerical propulsion system simulations (NPSS) project. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.

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35

Center, NASA Glenn Research, ed. Overview of high-fidelity modeling activities in the numerical propulsion system simulations (NPSS) project. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.

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36

Center, NASA Glenn Research, ed. Overview of high-fidelity modeling activities in the numerical propulsion system simulations (NPSS) project. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.

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37

United States. National Aeronautics and Space Administration., ed. Modeling improvements and users manual for axial-flow turbine off-design computer code AXOD. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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38

United States. National Aeronautics and Space Administration., ed. Design geometry and design/off-design performance computer codes for compressors and turbines. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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39

United States. National Aeronautics and Space Administration., ed. NASA Lewis Propulsion Systems Laboratory customer guide manual. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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40

United States. National Aeronautics and Space Administration., ed. NASA Lewis Propulsion Systems Laboratory customer guide manual. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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41

United States. National Aeronautics and Space Administration., ed. NASA Lewis Propulsion Systems Laboratory customer guide manual. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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42

Zuev, Sergey, Ruslan Maleev y Aleksandr Chernov. Energy efficiency of electrical equipment systems of autonomous objects. ru: INFRA-M Academic Publishing LLC., 2021. http://dx.doi.org/10.12737/1740252.

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Resumen
When considering the main trends in the development of modern autonomous objects (aircraft, combat vehicles, motor vehicles, floating vehicles, agricultural machines, etc.) in recent decades, two key areas can be identified. The first direction is associated with the improvement of traditional designs of autonomous objects (AO) with an internal combustion engine (ICE) or a gas turbine engine (GTD). The second direction is connected with the creation of new types of joint-stock companies, namely electric joint-stock companies( EAO), joint-stock companies with combined power plants (AOKEU). The energy efficiency is largely determined by the power of the generator set and the battery, which is given to the electrical network in various driving modes. Most of the existing methods for calculating power supply systems use the average values of disturbing factors (generator speed, current of electric energy consumers, voltage in the on-board network) when choosing the characteristics of the generator set and the battery. At the same time, it is obvious that when operating a motor vehicle, these parameters change depending on the driving mode. Modern methods of selecting the main parameters and characteristics of the power supply system do not provide for modeling its interaction with the power unit start-up system of a motor vehicle in operation due to the lack of a systematic approach. The choice of a generator set and a battery, as well as the concept of the synthesis of the power supply system is a problem studied in the monograph. For all those interested in electrical engineering and electronics.
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43

Ghodke, Chaitanya. Gas Turbine Blade Cooling. SAE International, 2018.

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44

Gas Turbine Blade Cooling. SAE International, 2018.

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45

Han, Je-Chin, Sandip Dutta y Srinath Ekkad. Gas Turbine Heat Transfer and Cooling Technology. CRC Press, 2012. http://dx.doi.org/10.1201/b13616.

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46

Han, Je-Chin, Sandip Dutta y Srinath Ekkad. Gas Turbine Heat Transfer and Cooling Technology. Taylor & Francis Group, 2012.

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47

Han, Je-Chin. Gas Turbine Heat Transfer and Cooling Technology. Taylor & Francis, 2001.

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48

Han, Je-Chin, Sandip Dutta y Srinath Ekkad. Gas Turbine Heat Transfer and Cooling Technology. Taylor & Francis Group, 2012.

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49

Prediction of film cooling on gas turbine airfoils. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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50

Gas Turbine System Technician (Electrical 3 & 2). United States Government Printing, 1985.

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