34th Congress of the International Council of the Aeronautical Sciences

04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance

NUMERICAL TOOLS FOR SLOW-GROWTH APPROACHES TO DAMAGE TOLERANT COMPOSITE AERONAUTICAL STRUCTURES

M. Khella¹, S. Ghiasvand¹, P. Ballarin¹, F. Panzeri¹, S. Piacquadio¹, A. Airoldi¹; ¹Politecnico di Milano, Italy

The activities presented are aimed at integrating in the same numerical approach both the prediction of the residual strength of a composite structural detail in the presence of damage and the evaluation of the crack growing rate under cyclic loading, so to represent a valuable tool for the design of damage tolerant composite aircraft and rotorcraft structures


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