An analytical model for the forced response of cyclic structures

Journal of Sound and Vibration

Volumn 209, Issue 3, 1998, Pages 531-536

  Turcotte, J S ^a  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DYNAMIC RESPONSE; EIGENVALUES AND EIGENFUNCTIONS; EQUATIONS OF MOTION; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; PARTIAL DIFFERENTIAL EQUATIONS;

CYCLIC STRUCTURES; FORCED RESPONSE; RECEPTANCE THEORY;

STRUCTURAL ANALYSIS;

EID: 0031695024     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.1997.1240     Document Type: Editorial

References (5)

1. D. J. EWINS 1973 Journal of Mechanical Engineering Science 15, 165-186. Vibration characteristics of bladed disk assemblies.
2. J. W. NICHOLSON 1986 American Institute of Aeronautics and Astronautics Journal 24, 485-491. Free vibration of stiffened rectangular plates using Green's functions and integral equations.
3. W. C. HURTY 1965 American Institute of Aeronautics and Astronautics Journal 3, 678-685. Dynamic analysis of structural systems using component modes.
4. L. MEIROVITCH 1967 Analytical Methods in Vibrations. New York: Macmillan Publishing Co.
5. C. PIERRE and D. V. MURTHY 1991 NASA technical memorandum 104519. Aeroelastic modal characteristics of mistuned blade assemblies: mode localization and loss of eigenstructure.