A coupled plate model of a bladed disk assembly

35th Joint Propulsion Conference and Exhibit

Volumn , Issue , 1999, Pages 1-11

  Turcotte, Jeffrey S ^a  

^a Air Force Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EIGENVALUES AND EIGENFUNCTIONS; MODAL ANALYSIS; NATURAL FREQUENCIES; PROPULSION; STIFFNESS MATRIX; VIBRATION ANALYSIS;

ADMISSIBLE FUNCTIONS; COMPONENT MODE SYNTHESIS; FORCED RESPONSE ANALYSIS; FREE AND FORCED VIBRATIONS; MISTUNED BLADED DISKS; RECTANGULAR PLATES; RESPONSE AMPLITUDES; STIFFNESS MATRICES;

TURBOMACHINE BLADES;

EID: 84963825551     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-2809     Document Type: Conference Paper

References (11)

1. Ewins, D. J., “Vibration Characteristics of Bladed Disk Assemblies,” Journal of Mechanical Engineering Science Vol. 15, 1973, pp. 165-186.
2. Shankar, K. and Keane, A. J., “A Study of the Vibrational Energies of Two Coupled Beams by Finite Element and Green Function (Recep-tance) Methods,” Journal of Sound and Vibration Vol. 181, 1995, pp. 801-838.
3. Turcotte, J. S., “An Analytical Model for the Forced Response of Cyclic Structures.” Journal of Sound and Vibration, Vol. 209,1998, pp. 531-536.
4. Turcotte, J. S., “Vibration of a Mistuned Blade-Disk Assembly Using Structurally Damped Beams,” 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, April 20-23 1998, Long Beach, CA.
5. Hollkamp, J. J., Hustedde, C. L., and Gordon, R. W., “Effects of Damping on a Blade-Disk Assembly,” 38th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, April 7-10, 1997, Kissimmee, FL.
6. Castanier, M. and Pierre, C., “Investigation of the Combined Effects of Intentional and Random Mistuning on the Forced Response of Bladed Disks,” 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 13-15, 1998, Cleveland, Ohio.
7. Slater, J., “Forced Response of Bladed Disk Assemblies-A Survey,” 34th AIAA/ASME/ SAE/ASEE Joint Propulsion Conference, July 13-15, 1998, Cleveland, Ohio.
8. Leissa, A. W., Vibration of Plates, NASA SP-160, National Aeronautics and Space Administration, Washington D. C., 1969.
9. Warburton, G. B., “The Vibration of Rectangular Plates,” Proceedings of the Institute of Mechanical Engineering, Serial A, Vol. 168, 1954, pp. 371-384.
10. Gordon, R. and Hollkamp, J., “An Experimental Investigation of Non-Uniform Damping in Blade-Disk Assemblies,” 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 13-15, 1998, Cleveland, Ohio.
11. Meirovitch, L., Analytical Methods in Vibrations, Macmillan Publishing, New York, 1976.