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

44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Volumn , Issue , 2003, Pages

  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

CLAMPED-CLAMPED BEAM; COMPARISON WITH EXPERIMENTS; COMPUTATIONAL BURDEN; COMPUTATIONAL EXPENSE; DIRECT TIME INTEGRATION; FINITE ELEMENT MODAL; NONLINEAR MODAL EQUATION; SONIC FATIGUE RESPONSE;

AIRCRAFT MANUFACTURE; AIRFRAMES; DYNAMIC RESPONSE; FINITE ELEMENT METHOD; FORECASTING; STRUCTURAL DYNAMICS;

NONLINEAR EQUATIONS;

EID: 84896851400     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

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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.