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1

Kiciński, Jan. Rotor dynamics. 2a 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. 2a ed. New York: J. Wiley, 1991.

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6

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

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7

I, Friswell M., a cura di. 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, e United States. National Aeronautics and Space Administration., a cura di. Nonlinear rotordynamics analysis. [Washington, D.C: National Aeronautics and Space Administration, 1986.

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12

Eliseo, DiRusso, Fleming David P e United States. National Aeronautics and Space Administration., a cura di. 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. e Ames Research Center, a cura di. 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, a cura di. 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 e United States. National Aeronautics and Space Administration., a cura di. 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, e United States. National Aeronautics and Space Administration., a cura di. 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. e Ames Research Center, a cura di. 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, a cura di. Rotordynamics prediction in engineering. 2a ed. Chichester: John Wiley, 1998.

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23

United States. Army Aviation Systems Command. e Ames Research Center, a cura di. 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., a cura di. 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, a cura di. Handbook of rotordynamics. New York: McGraw-Hill, 1992.

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27

United States. National Aeronautics and Space Administration., a cura di. 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 e United States. National Aeronautics and Space Administration., a cura di. 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 e United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, a cura di. 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, a cura di. History of Rotating Machinery Dynamics. Dordrecht: Springer Netherlands, 2011.

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42

Center, Ames Research, a cura di. 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, a cura di. 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, a cura di. 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, e Langley Research Center, a cura di. 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., a cura di. 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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