Nonlinear sonic fatigue response prediction from finite element modal models: A comparison with experiments

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 4, Issue , 2003, Pages 2796-2806

  Hollkamp, Joseph J ^a   Gordon, Robert W ^a   Spottswood, Stephen M ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTER SIMULATION; DYNAMIC RESPONSE; FATIGUE OF MATERIALS; FINITE ELEMENT METHOD; NONLINEAR EQUATIONS; RANDOM PROCESSES; STRUCTURAL DESIGN;

CALMPED-CLAMPED BEAM; NONLINEAR MODAL MODELS; NONLINEAR SONIC FATIGUE;

AIRCRAFT;

EID: 0042511913     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

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4. Rizzi S.A. and Muravyov A.A., "Equivalent Linearization Analysis of Geometrically Nonlinear Random Vibrations Using Commercial Finite Element Codes," NASA/TP-2002-211761, 2002.
5. Nash M., "Nonlinear Structural Dynamics by Finite Element Modal Synthesis", PhD. Dissertation, Imperial College, The University of London, 1977.
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8. McEwan M.I., "A Combined Modal / Finite Element Technique For The Non-Linear Dynamic Simulation Of Aerospace Structures", PhD Dissertation, Univ. of Manchester, England, 2001.
9. Gordon R.W., Hollkamp J.J, and Spottswood, S.M., "Nonlinear Response of a Clamped-Clamped Beam to Random Base Excitation," Proc. of the 8th Int. Conf. on Recent Advances in Structural Dynamics, University of South Hampton, July 2003.