The aircraft nacelle brace strength under some static types of loads
نویسندگان
چکیده
The problem of calculating the stress-strain state and solving weight optimization a single-engine transport aircraft nacelle fasteners is relevant In connection with development construction. One fastening elements brace, which under action static loads.. method calculation based on finite element method, considered in work. A tetrahedral was chosen as element. stresses strains brace were determined, analyzed recommendations for structural given.
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ژورنال
عنوان ژورنال: Mehanika giroskopi?eskih sistem
سال: 2022
ISSN: ['2519-2272', '0203-3771']
DOI: https://doi.org/10.20535/0203-3771422021269080