This study presents a comprehensive simulation and analysis of light aircraft landing gear models, focusing on dynamics and performance optimization. The landing gear of light aircraft plays a crucial role in ensuring safe landings and takeoffs, affecting both operational efficiency and passenger comfort. Through detailed modeling and simulation using advanced computational tools, various configurations and design parameters are evaluated to enhance landing gear performance under different operational conditions. The analysis includes considerations of structural integrity, shock absorption capabilities, and overall weight optimization to achieve improved reliability and efficiency. The findings contribute to the advancement of light aircraft design and safety standards, offering insights into future developments and enhancements in landing gear technology.

Landing gear dynamics, Aircraft safety, Structural analysis

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