The nonlinear response of shallow shells subjected to combined acoustic and thermal loads is analyzed using an efficient nonlinear modal finite element (FE) formulation. The acoustic loads have non-Gaussian probabilistic characteristics and are simulated by an algorithm capable of reliably converging to a target power spectral density (PSD) function and marginal probability density function (PDF). Factors contributing to the panel structural stiffness, softening and hardening effects, and modal contribution are also investigated along with their impact on the root-mean-square responses. The Palmgren–Miner cumulative damage theory in combination with the rainflow counting (RFC) cycles methods was used to estimate the panel fatigue life. Parametric studies for cylindrical and spherical curved panels considering stacking laminations, radii of curvatures, acoustic and thermal loads are studied in detail.
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March 2015
Research-Article
Fatigue Life of Curved Panels Under Combined Loading
Dhainaut Jean-Michel
Dhainaut Jean-Michel
Associate Professor of Mechanical Engineering
Mem. ASME
e-mail: dhain460@erau.edu
Mem. ASME
Embry Riddle Aeronautical University
,600 South Clyde Morris Blvd.
,Daytona Beach, FL 32114
e-mail: dhain460@erau.edu
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Dhainaut Jean-Michel
Associate Professor of Mechanical Engineering
Mem. ASME
e-mail: dhain460@erau.edu
Mem. ASME
Embry Riddle Aeronautical University
,600 South Clyde Morris Blvd.
,Daytona Beach, FL 32114
e-mail: dhain460@erau.edu
Contributed by the Design Engineering Division of ASME for publication in the JOURNAL OF COMPUTATIONAL AND NONLINEAR DYNAMICS. Manuscript received December 3, 2013; final manuscript received October 10, 2014; published online January 12, 2015. Assoc. Editor: Javier Garcia de Jalon.
J. Comput. Nonlinear Dynam. Mar 2015, 10(2): 021014 (8 pages)
Published Online: March 1, 2015
Article history
Received:
December 3, 2013
Revision Received:
October 10, 2014
Online:
January 12, 2015
Citation
Jean-Michel, D. (March 1, 2015). "Fatigue Life of Curved Panels Under Combined Loading." ASME. J. Comput. Nonlinear Dynam. March 2015; 10(2): 021014. https://doi.org/10.1115/1.4028802
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