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1

Kiciński, Jan. Rotor dynamics. 2nd ed. Gdańsk: Wydawn. IMP PAN, 2006.

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2

Krämer, Erwin. Dynamics of Rotors and Foundations. Berlin, Heidelberg: Springer Berlin Heidelberg, 1993. http://dx.doi.org/10.1007/978-3-662-02798-1.

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3

Dynamics of rotors and foundations. Berlin: Springer-Verlag., 1993.

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4

Krämer, Erwin. Dynamics of Rotors and Foundations. Berlin, Heidelberg: Springer Berlin Heidelberg, 1993.

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5

Rao, J. S. Rotor dynamics. 2nd ed. New York: J. Wiley, 1991.

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6

Rao, J. S. Rotor dynamics. 2nd ed. New Delhi: Wiley Eastern, 1991.

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7

I, Friswell M., ed. Fundamentals of rotor dynamics. New York: Cambridge University Press, 2010.

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8

Conference on Mechanical Vibration and Noise (12th 1989 Montreal, Quebec). Rotating machinery dynamics. New York, N.Y. (345 E. 47th St., New York 10017): American Society of Mechanical Engineers, 1989.

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9

International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (3rd 1990 Honolulu, Hawaii). Rotating machinery--dynamics: Proceedings of the Third International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-3). Washington: Hemisphere Pub. Corp., 1992.

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10

Rotordynamics. Boca Raton: Taylor & Francis, 2005.

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11

A, Zalick Richard, and United States. National Aeronautics and Space Administration., eds. Nonlinear rotordynamics analysis. [Washington, D.C: National Aeronautics and Space Administration, 1986.

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12

Eliseo, DiRusso, Fleming David P, and United States. National Aeronautics and Space Administration., eds. Active vibration control for flexible rotor by optimal direct-output feedback control. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.

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13

United States. Army Aviation Systems Command. and Ames Research Center, eds. Effects of blade-to-blade dissimilarities on rotor-body lead-lag dynamics. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

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14

F, Ehrich Fredric, ed. Handbook of rotordynamics. Malabar, FL: Krieger Pub. Co., 1999.

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15

Lakin, William D. CSM solutions of rotating blade dynamics using integrating matrices: Final report on NASA research grant NAG-1-1097, March 1, 1991 to February 28, 1992. [Washington, DC: National Aeronautics and Space Administration, 1992.

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16

Eliseo, DiRusso, Fleming David P, and United States. National Aeronautics and Space Administration., eds. Active vibration control for flexible rotor by optimal direct-output feedback control. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.

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17

Lalanne, M. Rotordynamics prediction in engineering. Chichester: Wiley, 1990.

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18

Chen, Robert T. N. An exploratory investigation of the flight dynamics effects of rotor RPM variations and rotor state feedback in hover. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

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19

A, Zalick Richard, and United States. National Aeronautics and Space Administration., eds. Nonlinear rotordynamics analysis. [Washington, D.C: National Aeronautics and Space Administration, 1991.

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20

Sopanen, Jussi. Studies of rotor dynamics using a multibody simulation approach. Lappeenranta: Lappeenranta University of Technology, 2004.

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21

United States. Army Aviation Systems Command. and Ames Research Center, eds. Effects of blade-to-blade dissimilarities on rotor-body lead-lag dynamics. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

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22

Guy, Ferraris, ed. Rotordynamics prediction in engineering. 2nd ed. Chichester: John Wiley, 1998.

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23

United States. Army Aviation Systems Command. and Ames Research Center, eds. Effects of blade-to-blade dissimilarities on rotor-body lead-lag dynamics. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

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24

United States. National Aeronautics and Space Administration., ed. Vibration control of rotor shaft systems by active control bearings. [Washington, D.C.]: National Aeronautics and Space Administration, 1985.

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25

Chen, Robert T. N. An exploratory investigation of the flight dynamics effects of rotor RPM variations and rotor state feedback in hover. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

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26

F, Ehrich Fredric, ed. Handbook of rotordynamics. New York: McGraw-Hill, 1992.

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27

United States. National Aeronautics and Space Administration., ed. Vibration control of rotor shaft systems by active control bearings. [Washington, D.C.]: National Aeronautics and Space Administration, 1985.

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28

Eliseo, DiRusso, Fleming David P, and United States. National Aeronautics and Space Administration., eds. Active vibration control for flexible rotor by optimal direct-output feedback control. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.

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29

Dynamics of rotor-bearing systems. London: Unwin Hyman, 1989.

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30

International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (3rd 1990 Honolulu, Hawaii). Rotating machinery--transport phenomena: Proceedings of the Third International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-3). Washington: Hemisphere Pub. Corp., 1992.

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31

Rieger, N. F. Balancing of rigid and flexible rotors. Washington, DC: Shock and Vibration Information Center, U.S. Dept. of Defense, 1986.

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32

Vance, John M. Machinery vibration and rotordynamics. Hoboken, N.J: Wiley, 2010.

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33

J, McNulty Michael, Bousman William G, Ames Research Center, United States Army, United States. Army Aviation Research and Technology Activity, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, eds. Integrated Technology Rotor Methodology Assessment Workshop: Proceedings of a workshop. Moffett Field, CA: US Army Aviation Systems Command, Aviation Research and Technology Activity, 1988.

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34

Conference on Mechanical Vibration and Noise (12th 1989 Montŕeal, Québec). Rotating machinery dynamics: Presented at the 1989 ASME Design Technical Conferences-12th Biennial Conference on Mechanical Vibration and Noise, Montreal, Quebec, Canada, September 17-21, 1989 ; sponsored by the Technical Committee on Vibration and Sound of the Design Engineering Division, ASME ; edited by T.S. Sankar ... [et al.]. New York, N.Y: American Society of Mechanical Engineers, 1989.

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35

Childs, Dara W. Turbomachinery rotordynamics: Phenomena, modeling, and analysis. New York: Wiley, 1993.

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36

International Conference on Rotor Dynamics (5th 1998 Darmstadt University of Technology). Proceedings of the Fifth International Conference on Rotor Dynamics. Braunschweig: Vieweg, 1998.

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37

International Conference on Rotor Dynamics (4th 1994 Chicago, Ill.). Proceedings of the Fourth International Conference on Rotor Dynamics, September 7-9, 1994, Chicago, USA. Willowbrook, Ill., USA: Vibration Institute, 1994.

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38

International Conference on Rotordynamics (3rd 1990 Lyon, France). Proceedings of 3rd International Conference on Rotordynamics: September 10-12, 1990, Lyon, France. Paris: Editions du Centre national de la recherche scientifique, 1990.

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39

Kiciński, Jan. Dynamika wirników i łożysk ślizgowych. Gdańsk: Wydawn. IMP PAN, 2000.

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40

Rotordynamics of turbomachinery. New York: Wiley, 1988.

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41

service), SpringerLink (Online, ed. History of Rotating Machinery Dynamics. Dordrecht: Springer Netherlands, 2011.

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42

Center, Ames Research, ed. Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

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43

Fejtek, Ian G. Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover. Washington, D. C: Ames Research Center, 1993.

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44

Center, Ames Research, ed. Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

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45

Center, Ames Research, ed. Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

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46

Chen, Robert T. N. A survey of nonuniform inflow models for rotorcraft flight dynamics and control applications. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

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47

Chen, Robert T. N. A survey of nonuniform inflow models for rotorcraft flight dynamics and control applications. Moffett Field, Calif: Ames Research Center, 1989.

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48

A, Silva Walter, and Langley Research Center, eds. The effects of aeroelastic deformation on the unaugmented stopped-rotor dynamics of an x-wing aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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49

International Symposium on Transport Phenomena, Dynamics, and Design of Rotating Machinery (2nd 1988 Honolulu, Hawaii). Dynamics of rotating machinery: Proceedings of the Second International Symposium on Transport Phenomena, Dynamics, and Design of Rotating Machinery, part II. New York: Hemisphere Pub. Corp., 1990.

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50

United States. National Aeronautics and Space Administration., ed. An experimental and theoretical comparison of rotordynamic coefficients for sawtooth-pattern damper seals. College Station, Tex: Turbomachinery Laboratories, Mechanical Engineering Dept., Texas A & M University, 1987.

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