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Books on the topic 'Turbine blade cooling'

Author: Grafiati
Published: 4 June 2021
Last updated: 25 July 2025

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1

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

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2

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

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3

Noot, Marc. Numerical analysis of turbine blade cooling ducts. Eindhoven University, 1997.

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4

Garg, Vijay Kumar. Leading edge film cooling effects on turbine blade heat transfer. National Aeronautics and Space Administration, 1995.

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5

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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6

-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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7

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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8

M, Russell Louis, and Lewis Research Center, eds. Measurements of heat transfer, flow, and pressures in a simulated turbine blade internal cooling passage. National Aeronautics and Space Administration, Lewis Research Center, 1997.

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9

M, Russell Louis, and Lewis Research Center, eds. Measurements of heat transfer, flow, and pressures in a simulated turbine blade internal cooling passage. National Aeronautics and Space Administration, Lewis Research Center, 1997.

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10

M, Russell Louis, and United States. National Aeronautics and Space Administration., eds. Measurements and computational analysis of heat transfer and flow in a simulated turbine blade internal cooling passage. National Aeronautics and Space Administration, 1993.

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11

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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12

Abdul-Aziz, Ali. Design evaluation using finite element analysis of cooled silicon nitride plates for a turbine blade application. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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13

Abdul-Aziz, Ali. Design evaluation using finite element analysis of cooled silicon nitride plates for a turbine blade application. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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14

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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15

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

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16

Bogomolov, E. N. Rabochie prot͡s︡essy v okhlazhdaemykh turbinakh gazoturbinnykh dvigateleĭ s perforirovannymi lopatkami. Mashinostroenie, 1987.

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17

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

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18

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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19

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

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20

Philip, Poinsatte, NASA Glenn Research Center, and U.S. Army Research Laboratory., eds. Experimental heat transfer and bulk air temperature measurements for a multipass internal cooling model with ribs and bleed. National Aeronautics and Space Administration, Glenn Research Center, 2000.

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21

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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22

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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23

E, Gaugler R., and United States. National Aeronautics and Space Administration., eds. Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades. National Aeronautics and Space Administration, 1997.

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24

Garg, Vijay Kumar. Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades. National Aeronautics and Space Administration, 1995.

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25

Symposium of the AGARD Propulsion and Energetics Panel (65th 1985 Bergen, Norway). Heat transfer and cooling in gas turbines: Papers presented at the Propulsion and Energetics Panel 65th Symposium, held in Bergen, Norway, 6-10 May 1985. North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development, 1985.

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26

A, Ameri Ali, Rigby David L, and United States. National Aeronautics and Space Administration., eds. Simulations of turbine cooling flows using a multiblock-multigrid scheme: Under cooperative agreement NCC3-370. National Aeronautics and Space Administration, 1996.

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27

A, Ameri Ali, Rigby David L, and United States. National Aeronautics and Space Administration., eds. Simulations of turbine cooling flows using a multiblock-multigrid scheme: Under cooperative agreement NCC3-370. National Aeronautics and Space Administration, 1996.

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28

A, Ameri Ali, Rigby David L, and United States. National Aeronautics and Space Administration., eds. Simulations of turbine cooling flows using a multiblock-multigrid scheme: Under cooperative agreement NCC3-370. National Aeronautics and Space Administration, 1996.

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29

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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30

Gary, Steuber, and United States. National Aeronautics and Space Administration., eds. Flow in rotating serpentine coolant passages with skewed trip strips: Under contract NAS3-27378. National Aeronautics and Space Administration, 1996.

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31

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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32

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

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33

Gas Turbine Blade Cooling. SAE International, 2018.

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34

Air Cooling of a Slotted Gas Turbine Blade. Creative Media Partners, LLC, 2021.

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35

The effect of wake passing on turbine blade film cooling. National Aeronautics and Space Administration, 1996.

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36

National Aeronautics and Space Administration (NASA) Staff. Effect of Film-Hole Shape on Turbine Blade Film Cooling Performance. Independently Published, 2018.

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37

National Aeronautics and Space Administration (NASA) Staff. Analysis of Turbine Blade Relative Cooling Flow Factor Used in the Subroutine Coolit Based on Film Cooling Correlations. Independently Published, 2019.

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38

Effect of Blade Cooling on Performance of a Gas Turbine Power Plant. Creative Media Partners, LLC, 2021.

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39

Kreatsoulas, J. C. Effects of rotation on impingement cooling of turbine blades. 1985.

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40

Survey of Advantages and Problems Associated with Transpiration Cooling and Film Cooling of Gas-Turbine Blades. Creative Media Partners, LLC, 2021.

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41

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

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