Development of composite torsion shaft for the aircraft structure under multiple load condition
نویسندگان
چکیده
منابع مشابه
“ Finite Element & Experimental Investigation of Composite Torsion Shaft ”
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ژورنال
عنوان ژورنال: Journal of the Korean Society for Aeronautical & Space Sciences
سال: 2016
ISSN: 1225-1348
DOI: 10.5139/jksas.2016.44.6.484