Books on the topic 'Turbomachinery measurements'

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1

Gahagan, Shane G. Pressure-sensitive paint measurements on a rotor disk surface at high speeds. Monterey, Calif: Naval Postgraduate School, 1997.

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2

United States. National Aeronautics and Space Administration., ed. Data reduction procedures for laser velocimeter measurements in turbomachinery rotors. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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3

Quinn, Kevin J. Pressure-sensitive paint measurement technique development for turbomachinery application. Monterey, Calif: Naval Postgraduate School, 1997.

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4

Goldman, Louis J. Three-component laser anemometer measurement systems. Cleveland, Ohio: Lewis Research Center, 1991.

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5

Barranger, John P. Low-cost FM oscillator for capacitance type of blade tip clearance measurement system. Cleveland, Ohio: Lewis Research Center, 1987.

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6

Dickinson, Wayne. A benthic chamber with electric stirrer mixing. Woods Hole, Mass: Woods Hole Oceanographic Institution, 1992.

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7

Elsner, Janusz W. Metrologia turbulencji przepływów. Wrocław: Zakład Narodowy im. Ossolińskich, 1995.

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8

King, Paul I. Testing, analysis, and code verification of aerodynamics and heat transfer related to turbomachinery: Final report. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1991.

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9

King, Paul I. Testing, analysis, and code verification of aerodynamics and heat transfer related to turbomachinery: Final report. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1991.

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10

Kurkov, Anatole P. Measurement of gust response on a turbine cascade. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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11

Harris, D. L. Measurement of damping of composite materials for turbomachinery applications: (MSFC Center director's discretionary fund final report, project no. 94-05). [Washington, D.C: National Aeronautics and Space Administration, 1998.

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12

United States. National Aeronautics and Space Administration., ed. Data reduction procedures for laser velocimeter measurements in turbomachinery rotors. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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13

S, Dhadwal Harbans, and NASA Glenn Research Center, eds. Simultaneous optical measurements of axial and tangential steady-state blade deflections. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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14

S, Dhadwal Harbans, and NASA Glenn Research Center, eds. Simultaneous optical measurements of axial and tangential steady-state blade deflections. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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15

Ramp-integration technique for capacitance-type blade-tip clearance measurement. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

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16

P, Barranger John, and Lewis Research Center, eds. Ramp-integration technique for capacitance-type blade-tip clearance measurement. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

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17

United States. National Aeronautics and Space Administration., ed. Recent advances in capacitance type blade tip clearance measurements. [Washington, D.C.]: National Aeronautics and Space Administration, 1988.

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18

United States. National Aeronautics and Space Administration., ed. PIV for turbomachinery applications. [Washington, D.C: National Aeronautics and Space Administration, 1997.

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19

Pressure-Sensitive Paint Measurement Technique Development for Turbomachinery Application. Storming Media, 1997.

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20

National Aeronautics and Space Administration (NASA) Staff. Measurement of Damping of Composite Materials for Turbomachinery Applications. Independently Published, 2018.

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21

V, Brown Gerald, and United States. National Aeronautics and Space Administration., eds. A low-cost optical data acquisition system for vibration measurement. [Washington, DC]: National Aeronautics and Space Administration, 1987.

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22

V, Brown Gerald, and United States. National Aeronautics and Space Administration., eds. A low-cost optical data acquisition system for vibration measurement. [Washington, DC]: National Aeronautics and Space Administration, 1987.

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23

V, Brown Gerald, and United States. National Aeronautics and Space Administration., eds. A low-cost optical data acquisition system for vibration measurement. [Washington, DC]: National Aeronautics and Space Administration, 1987.

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24

Three-component laser anemometer measurement systems. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

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25

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Three-component laser anemometer measurement systems. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

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26

P, Kurkov A., Janetzke David C, and NASA Glenn Research Center, eds. Time-of-flight tip-clearance measurements. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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27

P, Kurkov A., Janetzke D. C, and NASA Glenn Research Center, eds. Time-of-flight tip-clearance measurements. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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28

P, Kurkov A., Janetzke David C, and NASA Glenn Research Center, eds. Time-of-flight tip-clearance measurements. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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29

Time-of-flight tip-clearance measurements. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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30

Structural dynamic measurement practices for turbomachinery at the NASA Lewis Research Center. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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31

Center, Lewis Research, ed. PSP measurement of stator vane surface pressures in a high speed fan. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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32

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., ed. Low-cost FM oscillator for capacitance type of blade tip clearance measurement system. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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33

Low-cost FM oscillator for capacitance type of blade tip clearance measurement system. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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34

Low-cost FM oscillator for capacitance type of blade tip clearance measurement system. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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35

D, Quinn Roger, Kadambi Jaikrishnan R, and United States. National Aeronautics and Space Administration., eds. The practical implementation of non-contacting laser strain measurement systems. [Washington, D.C: National Aeronautics and Space Administration, 2000.

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36

D, Quinn Roger, Kadambi Jaikrishnan R, and United States. National Aeronautics and Space Administration., eds. The practical implementation of non-contacting laser strain measurement systems. [Washington, D.C: National Aeronautics and Space Administration, 2000.

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37

United States. National Aeronautics and Space Administration., ed. Measurement of damping of composite materials for turbomachinery applications: (MSFC Center director's discretionary fund final report, project no. 94-05). [Washington, D.C: National Aeronautics and Space Administration, 1998.

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38

Walker, Duncan. Torsional Vibration of Turbo-Machinery. McGraw-Hill Professional, 2003.

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39

Torsional Vibration of Turbo-Machinery. McGraw-Hill Professional, 2003.

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40

United States. National Aeronautics and Space Administration. and United States. Army Aviation Systems Command., eds. Unsteady flows in a single-stage transonic axial-flow fan stator row. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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