COMPARISON OF GLOBAL AND LOCAL MODELS OF AIRCRAFT LANDING NOSE LAMP CUT-OFF
DOI:
https://doi.org/10.30890/2709-1783.2025-40-00-022Keywords:
global model, stress-strain state, landing gear strut, fuselage, stiffeners, finite elementsAbstract
This paper develops a global model of the nose landing gear compartment of an aircraft, presents calculations of the stress-strain state of the structure using the PATRAN/NASTRAN software package based on the MFE [1], and compares the calculation results
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2025-08-30
How to Cite
Levytska, T., Pozhuieva, I., & Manzhos, O. (2025). COMPARISON OF GLOBAL AND LOCAL MODELS OF AIRCRAFT LANDING NOSE LAMP CUT-OFF. SWorld-Ger Conference Proceedings, 1(gec40-00), 21–24. https://doi.org/10.30890/2709-1783.2025-40-00-022
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