Monte Carlo Simulation Methodology for the Reliability of Aircraft Structures
Andreas Rambalakos
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Monte Carlo Simulation Methodology for the Reliability of Aircraft Structures

Reliability of Aircraft Structures Under Damage Tolerance Requirements

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Aviation rules mandate the need for an aircraft structure to meet damage tolerance requirements. The damaged structure must maintain adequate residual strength in order to maintain its integrity and this is accomplished through a continuous inspection program. The multifold objective of this work is to present a methodology based on a direct Monte Carlo simulation (MCS) process to assess the reliability of an aircraft structure. Initially, the structure is modeled as a parallel system with active redundancy comprised of elements with uncorrelated strengths. Closed form expressions for the syst...