Książki na temat „Rotors – Dynamics”
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Kiciński, Jan. Rotor dynamics. Wyd. 2. Gdańsk: Wydawn. IMP PAN, 2006.
Znajdź pełny tekst źródłaKrämer, Erwin. Dynamics of Rotors and Foundations. Berlin, Heidelberg: Springer Berlin Heidelberg, 1993. http://dx.doi.org/10.1007/978-3-662-02798-1.
Pełny tekst źródłaDynamics of rotors and foundations. Berlin: Springer-Verlag., 1993.
Znajdź pełny tekst źródłaKrämer, Erwin. Dynamics of Rotors and Foundations. Berlin, Heidelberg: Springer Berlin Heidelberg, 1993.
Znajdź pełny tekst źródłaRao, J. S. Rotor dynamics. Wyd. 2. New York: J. Wiley, 1991.
Znajdź pełny tekst źródłaRao, J. S. Rotor dynamics. Wyd. 2. New Delhi: Wiley Eastern, 1991.
Znajdź pełny tekst źródłaI, Friswell M., red. Fundamentals of rotor dynamics. New York: Cambridge University Press, 2010.
Znajdź pełny tekst źródłaConference 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.
Znajdź pełny tekst źródłaInternational 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.
Znajdź pełny tekst źródłaRotordynamics. Boca Raton: Taylor & Francis, 2005.
Znajdź pełny tekst źródłaA, Zalick Richard, i United States. National Aeronautics and Space Administration., red. Nonlinear rotordynamics analysis. [Washington, D.C: National Aeronautics and Space Administration, 1986.
Znajdź pełny tekst źródłaEliseo, DiRusso, Fleming David P i United States. National Aeronautics and Space Administration., red. Active vibration control for flexible rotor by optimal direct-output feedback control. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.
Znajdź pełny tekst źródłaUnited States. Army Aviation Systems Command. i Ames Research Center, red. Effects of blade-to-blade dissimilarities on rotor-body lead-lag dynamics. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.
Znajdź pełny tekst źródłaF, Ehrich Fredric, red. Handbook of rotordynamics. Malabar, FL: Krieger Pub. Co., 1999.
Znajdź pełny tekst źródłaLakin, 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.
Znajdź pełny tekst źródłaEliseo, DiRusso, Fleming David P i United States. National Aeronautics and Space Administration., red. Active vibration control for flexible rotor by optimal direct-output feedback control. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.
Znajdź pełny tekst źródłaLalanne, M. Rotordynamics prediction in engineering. Chichester: Wiley, 1990.
Znajdź pełny tekst źródłaChen, 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.
Znajdź pełny tekst źródłaA, Zalick Richard, i United States. National Aeronautics and Space Administration., red. Nonlinear rotordynamics analysis. [Washington, D.C: National Aeronautics and Space Administration, 1991.
Znajdź pełny tekst źródłaSopanen, Jussi. Studies of rotor dynamics using a multibody simulation approach. Lappeenranta: Lappeenranta University of Technology, 2004.
Znajdź pełny tekst źródłaUnited States. Army Aviation Systems Command. i Ames Research Center, red. Effects of blade-to-blade dissimilarities on rotor-body lead-lag dynamics. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.
Znajdź pełny tekst źródłaGuy, Ferraris, red. Rotordynamics prediction in engineering. Wyd. 2. Chichester: John Wiley, 1998.
Znajdź pełny tekst źródłaUnited States. Army Aviation Systems Command. i Ames Research Center, red. Effects of blade-to-blade dissimilarities on rotor-body lead-lag dynamics. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. Vibration control of rotor shaft systems by active control bearings. [Washington, D.C.]: National Aeronautics and Space Administration, 1985.
Znajdź pełny tekst źródłaChen, 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.
Znajdź pełny tekst źródłaF, Ehrich Fredric, red. Handbook of rotordynamics. New York: McGraw-Hill, 1992.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. Vibration control of rotor shaft systems by active control bearings. [Washington, D.C.]: National Aeronautics and Space Administration, 1985.
Znajdź pełny tekst źródłaEliseo, DiRusso, Fleming David P i United States. National Aeronautics and Space Administration., red. Active vibration control for flexible rotor by optimal direct-output feedback control. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.
Znajdź pełny tekst źródłaDynamics of rotor-bearing systems. London: Unwin Hyman, 1989.
Znajdź pełny tekst źródłaInternational 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.
Znajdź pełny tekst źródłaRieger, N. F. Balancing of rigid and flexible rotors. Washington, DC: Shock and Vibration Information Center, U.S. Dept. of Defense, 1986.
Znajdź pełny tekst źródłaVance, John M. Machinery vibration and rotordynamics. Hoboken, N.J: Wiley, 2010.
Znajdź pełny tekst źródłaJ, McNulty Michael, Bousman William G, Ames Research Center, United States Army, United States. Army Aviation Research and Technology Activity i United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, red. Integrated Technology Rotor Methodology Assessment Workshop: Proceedings of a workshop. Moffett Field, CA: US Army Aviation Systems Command, Aviation Research and Technology Activity, 1988.
Znajdź pełny tekst źródłaConference 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.
Znajdź pełny tekst źródłaChilds, Dara W. Turbomachinery rotordynamics: Phenomena, modeling, and analysis. New York: Wiley, 1993.
Znajdź pełny tekst źródłaInternational Conference on Rotor Dynamics (5th 1998 Darmstadt University of Technology). Proceedings of the Fifth International Conference on Rotor Dynamics. Braunschweig: Vieweg, 1998.
Znajdź pełny tekst źródłaInternational 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.
Znajdź pełny tekst źródłaInternational 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.
Znajdź pełny tekst źródłaKiciński, Jan. Dynamika wirników i łożysk ślizgowych. Gdańsk: Wydawn. IMP PAN, 2000.
Znajdź pełny tekst źródłaRotordynamics of turbomachinery. New York: Wiley, 1988.
Znajdź pełny tekst źródłaservice), SpringerLink (Online, red. History of Rotating Machinery Dynamics. Dordrecht: Springer Netherlands, 2011.
Znajdź pełny tekst źródłaCenter, Ames Research, red. 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.
Znajdź pełny tekst źródłaFejtek, Ian G. Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover. Washington, D. C: Ames Research Center, 1993.
Znajdź pełny tekst źródłaCenter, Ames Research, red. 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.
Znajdź pełny tekst źródłaCenter, Ames Research, red. 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.
Znajdź pełny tekst źródłaChen, 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.
Znajdź pełny tekst źródłaChen, Robert T. N. A survey of nonuniform inflow models for rotorcraft flight dynamics and control applications. Moffett Field, Calif: Ames Research Center, 1989.
Znajdź pełny tekst źródłaA, Silva Walter, i Langley Research Center, red. 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.
Znajdź pełny tekst źródłaInternational 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.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. 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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