Optimum Design of Symmetric Laminated Reinforced Plate Subjected to in-Plane Compressive Loading: Buckling Analysis
نویسندگان
چکیده
ثد لانبد نم دهلا ليد لا د ا س ندده نل ا لا نةادد لانملي داملنجيدع ن ميديللأي ن ن. بإ ن ن دم ن د اعينملي دالانادمالنجيدع نلاانلد نهيجاا, ي الانا ُن, هجادلان نن ن ضا لاندنتا سيغا لانب ن د ج مييلأ ن ن دك لاندن يقسلانملي الا نسي رداندن ديمكلان ي داملن ن جيددع نلاانلدد ن دد نيددهب سن ددانتا سدديغا لانهيددهن. ددي د لانمدسددظلا ن نسدداينعلانن يددنس ن ا صادد ي نملي ددالانبدد ن دد نلدديم ا ناددليند نة لا ANSYS ن ن جدنث لانللاصنب ن. بإ ن لضفأ ن نبياسا مييللأل ن نةاد ن ي ال مييللأي ن نتاي ين إ ن نددهنةيدفي لان دي جلنبي ن يدا ز 45 د ن ن دهجادلانبد ننتايناي د لاان دي جل 1 ند 2 ن ن د د لان دلي ن د فن. دي د لانمدسدظلانسدييغان دن ن دلي لانهيدهنسديغااندن, بي بي ت نبياسالانبيكنت +30/-30 ن نبياسالانده لي لا ن ن دلي ن دفنيد ني ن, دهجادلانبد نن ي جلندنجيع نلاان دي ن ف ةس ن د لا ن تد تد نبدياسالانبيدكننتد +15/-15 ن ندده لدضفلأا نةسدكيد لانتلايد لان دي جلندن. هلاد أ نجيدع نلاانلد ن ا زدين, ن دن هجادلان ننة ييزن ة ييزن ن يكرالي ن نن. ي الانا ُ ن Abstract:
منابع مشابه
Buckling analysis of quasi-isotropic symmetrically laminated rectangular composite plates with an elliptical/circular cutout subjected to linearly varying in-plane loading using fem
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