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1

Hendricks, Robert C. Straight cylindrical seal for high-performance turbomachines. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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2

Hendricks, Robert C. Straight cylindrical seal for high-performance turbomachines. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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3

Hendricks, Robert C. Three-step cylindrical seal for high-performance turbomachines. Lewis Research Center, 1987.

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4

Hendricks, Robert C. Three-step cylindrical seal for high-performance turbomachines. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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5

Hendricks, Robert C. Three-step cylindrical seal for high-performance turbomachines. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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6

Wislicenus, George F. Preliminary design of turbopumps and related machinery. NASA, Scientific and Technical Information Branch, 1986.

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7

Wislicenus, George F. Preliminary design of turbopumps and related machinery. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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8

Armstrong, Elizabeth S. Computer-aided design analysis of 57-mm, angular-contact, cryogenic turbopump bearings. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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9

Armstrong, Elizabeth S. Computer-aided design analysis of 57-mm, angular-contact, cryogenic turbopump bearings. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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10

Armstrong, Elizabeth S. Computer-aided design analysis of 57-mm, angular-contact, cryogenic turbopump bearings. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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11

Armstrong, Elizabeth S. Computer-aided design analysis of 57-mm, angular-contact, cryogenic turbopump bearings. Lewis Research Center, 1988.

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12

Boretti, A. A. Transonic viscous flow calculations for a turbine cascade with a two equation turbulence model. National Aeronautics and Space Administration, 1989.

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13

Martinez-Sanchez, Manuel. Phase III report on contract number NAS8-35018 entitled Turbine blade tip and seal clearance excitation forces. National Aeronautics and Space Administration, 1992.

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14

Hendricks, Robert C. Three-step labyrinth seal for high-performance turbomachines. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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15

Hendricks, Robert C. Three-step labyrinth seal for high-performance turbomachines. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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16

Hendricks, Robert C. Three-step labyrinth seal for high-performance turbomachines. Lewis Research Center, 1987.

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17

Parsons International Turbine Conference (2nd 1984 Churchill College). Materials development in Turbo-machinery design: Second Parsons International Turbine Conference. Institute of Metals, 1989.

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18

Cunningham, Robert E. Passive eddy-current damping as a means of vibration control in cryogenic turbomachinery. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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19

E, Cunningham Robert. Passive eddy-current damping as a means of vibration control in cryogenic turbomachinery. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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20

Cunningham, Robert E. Passive eddy-current damping as a means of vibration control in cryogenic turbomachinery. Lewis Research Center, 1986.

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21

Choo, Yung K. Generation of a composite grid for turbine flows and consideration of a numerical scheme. National Aeronautics and Space Administration, 1987.

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22

Martinez-Sanchez, Manuel. Turbine blade-tip clearance excitation forces: Final report on Contract number NAS8-35018. Massachusetts Institute of Technology, 1985.

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23

Martinez-Sanchez, Manuel. Turbine blade-tip clearance excitation forces: Final report on Contract number NAS8-35018. Massachusetts Institute of Technology, 1985.

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24

Pietraszkiewicz, Wojciech. 50 lat Instytutu Maszyn Przepływowych im R. Szewalskiego Polskiej Akademii Nauk w Gdańsku: Księga jubileuszowa. Instytut Maszyn Przepływowych PAN, 2000.

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25

Milner, Edward J. Simulating a small turboshaft engine in a real-time multiprocessor simulator (RTMPS) environment. National Aeronautics and Space Administration, Lewis Research Center, 1986.

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26

International Joint Power Generation Conference (1990 Boston, Mass.). Cogeneration and combined cycle plants--design, interconnection, and turbine applications: Presented at the 1990 International Joint Power Generation Conference, Boston, Massachusetts, October 21-25, 1990. American Society of Mechanical Engineers, 1990.

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27

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., ed. Three-step cylindrical seal for high-performance turbomachines. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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28

Troubleshooting Rotating Machinery: Including Centrifugal Pumps and Compressors, Reciprocating Pumps and Compressors, Fans, Steam Turbines, Electric Motors, and More. Wiley & Sons, Incorporated, John, 2016.

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29

Perez, Robert X., and Andrew P. Conkey. Troubleshooting Rotating Machinery: Including Centrifugal Pumps and Compressors, Reciprocating Pumps and Compressors, Fans, Steam Turbines, Electric Motors, and More. Wiley & Sons, Incorporated, John, 2016.

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30

United States. National Aeronautics and Space Administration., ed. Turbomachinery rotor forces: Final report, contract NAS8-33108 (October 30, 1978 - August 30, 1988). California Institute of Technology, Division of Engineering and Applied Science, 1988.

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31

C, Young William, Roberton Reginald S, and ASTM Committee D-2 on Petroleum Products and Lubricants., eds. Turbine oil monitoring. ASTM, 1989.

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32

Gas Turbine Engineering Handbook, Second Edition (Incompressible Flow Turbomachines). 2nd ed. Gulf Professional Publishing, 2001.

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33

Center, Ames Research, ed. Three-dimensional Navier-Stokes simulations of turbine rotor-stator interaction. National Aeronautics and Space Administration, Ames Research Center, 1988.

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34

Three-dimensional Navier-Stokes simulations of turbine rotor-stator interaction. National Aeronautics and Space Administration, Ames Research Center, 1988.

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35

Center, Ames Research, ed. Three-dimensional Navier-Stokes simulations of turbine rotor-stator interaction. National Aeronautics and Space Administration, Ames Research Center, 1988.

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36

Forsthoffer, William. Forsthoffer's Rotating Equipment Handbooks, Vol. 2: Pumps (Forsthoffer's Rotating Equipment Handbooks). Elsevier Science, 2005.

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37

Forsthoffer, William. Forsthoffer's Rotating Equipment Handbooks, Vol. 1: Fundamentals of Rotating Equipment (World Pumps). Elsevier Science, 2005.

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38

A comparison of the analytical and experimental performance of the solid version of a cooled radial turbine. National Aeronautics and Space Administration, 1991.

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39

Escudier, Marcel. Introduction to Engineering Fluid Mechanics. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198719878.001.0001.

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Turbojet and turbofan engines, rocket motors, road vehicles, aircraft, pumps, compressors, and turbines are examples of machines which require a knowledge of fluid mechanics for their design. The aim of this undergraduate-level textbook is to introduce the physical concepts and conservation laws which underlie the subject of fluid mechanics and show how they can be applied to practical engineering problems. The first ten chapters are concerned with fluid properties, dimensional analysis, the pressure variation in a fluid at rest (hydrostatics) and the associated forces on submerged surfaces, t
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40

Composite grid and finite-volume LU implicit scheme for turbine flow analysis. National Aeronautics and Space Administration, 1987.

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41

George C. Marshall Space Flight Center., ed. Comprehensive structural dynamic analysis of the SSME/AT fuel pump first-stage turbine blade. National Aeronautics and Space Administration, Marshall Space Flight Center, 1998.

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42

M, Greitzer Edward, George C. Marshall Space Flight Center., and Massachusetts Institute of Technology, eds. Turbine blade-tip clearance excitation forces: Final report on Contract number NAS8-35018. Massachusetts Institute of Technology, 1985.

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43

M, Greitzer Edward, George C. Marshall Space Flight Center, and Massachusetts Institute of Technology, eds. Turbine blade-tip clearance excitation forces: Final report on Contract number NAS8-35018. Massachusetts Institute of Technology, 1985.

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