In this study, it was aimed to design a composite landing gear that is resistant to landing loads and has maximum lightness in unmanned aerial vehicles. In this context, a landing gear design was carried out based on the loads that the aircraft's landing gear will be exposed to during landing and take-off, and a three-dimensional modeling was created. Numerical analyzes were made using the designed solid model finite element method. It has been observed that the obtained data can meet the loads on the aircraft landing gear in the specified configuration without any breakage. The findings at the end of the study were supported by graphics.
Research Article
Keywordsana iniş takımı, dikme, sonlu analiz