The crack path in fuselage panel under mixed mode biaxial loading
نویسندگان
چکیده
منابع مشابه
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ژورنال
عنوان ژورنال: Frattura ed Integrità Strutturale
سال: 2019
ISSN: 1971-8993
DOI: 10.3221/igf-esis.48.11