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Article
Linear Damage Rule Life Prediction for Stress Controlled Fatigue-Creep Interaction of Aluminum Alloys
تخمین عمر الضرر الخطي للاجھاد المسیطر لتداخل الكلال والزحف لسبائك الالمنیوم

Authors: Salah F. Abd-El-Jabbar --- Shakir Sakran Hassan --- Hussain J. Al-Alkawi
Journal: Engineering and Technology Journal مجلة الهندسة والتكنولوجيا ISSN: 16816900 24120758 Year: 2012 Volume: 30 Issue: 5 Pages: 729-743
Publisher: University of Technology الجامعة التكنولوجية

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Abstract

The fatigue-creep interaction performance of 5086 and 6061-T651 aluminumalloys were investigated for specimens tested under control stress rotating bending at a stress ratio R=-1 and 250°C temperature. The fatigue endurance limit for both alloys reduced at 250°C.The fatigue and creep damage was evaluated based on the linear damage rule, where the fatigue damage was determined as the number of cycles to failure and the creep damage was evaluated based on the time applied experimentally for low to high and high to low amplitude stress. The cumulative fatigue-creep interaction damage was found to around 0.5 i.e DF +Dc =0.5 Fatigue – creep interaction lives predicted by the linear damage rule were compared to the actual lives. The results show that the linear damage rule gave an overestimated predictions.


Article
The influence of the temperature on the ultimate tensile strength of the composite materials at constant Fiber volume fraction
تأثيردرجة الحرارة على مقاومة الشد للمواد المتراكبة بثبوت الكسر الحجمي للألياف

Authors: Hussain J. Al-alkawi --- Dhafir S. Al-Fattal --- Abdul-jabar H. Ali
Journal: Engineering and Technology Journal مجلة الهندسة والتكنولوجيا ISSN: 16816900 24120758 Year: 2012 Volume: 30 Issue: 11 Pages: 1935-1947
Publisher: University of Technology الجامعة التكنولوجية

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Abstract

The aim of this work is to study the influence of the temperature on the ultimatetensile strength (UTS) of composite material which is manufactured from polyester andE-glass (woven roving, chopped strand mat) as a laminate with a constant fiber volumefraction (VF) of 33%. The results showed a little effect of temperature on tensilestrength in the range of room temperature (RT) to 50 oC for laminates reinforced withE-glass (woven roving) [0/90, ±45,0/90], [0/90]3, and [0/90, CSM, 0/90], but forlaminates reinforced with E-glass chopped strand mat (CSM), as [CSM] 3 and [CSM,0/90, CSM], a continuous reduction in strength was observed with increasingtemperature from (RT) to 60 oC. The highest percentage reduction in strength was 23%at 60oC as compared with (RT) for [CSM]3 laminate

بهدف هذا البحث الى دراسة تأثير درجات الحراره على مقاومةالشد للمواد المتراكبه المصنعه من البولستر والالياف الزجاجيه وبنسبه حجميه ثابتة للألياف الزجاجية مقدارها 33 %. أظهرت نتائج 0/90 ] تتأثر قليلا ]3 ,[0/90, CSM, 0/90], [0/90, ±45, 0/ البحث ان المواد المصنعه من ,[ 90 بدرجات الحراره ما في مدى ( درجة حرارة الغرفة و 50 درجه مئويه) في حين ان المواد المصنعه تظهر انخفاض مستمر في اجهاد الشد الاقصى مع زيادة [CSM]3 ,[CSM, 0/90, CSM] من درجة الحراره من درجه حرارة الغرفة الى 60 درجه مئويه وان اعلى نسبة انخفاض لمقاومة الشد كان مقدارها 23 % وذلك عند 60 درجه مئويه مقارنة بمقاومة الشد عند درجه حرارة الغرفة وللماده . [CSM] المصنعه من 3


Article
Types of the Fiber Glass-Mat on Fatigue Characteristic of Composite Materials at Constant Fiber Volume Fraction: Experimental Determination
تأثير نوع حصيرة الا لياف الزجاجية على سلوك الكلال للمواد المتراكبة عند نسبة حجميه ثابتة للالياف الزجاجية

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Abstract

The aim of this work is to study the influence of the type of fiber glass –mat on fatigue behavior of composite material which is manufactured from polyester and E-glass (woven roving, chopped strand mat (CSM)) as a laminate with a constant fiber volume fraction (VF) of 33%. The results showed that the laminates reinforced with E-glass (woven roving) [0/90, ±45.0/90] and [0/90, CSM, 0/90] have lower fatigue strength than the laminates reinforced with E-glass [0/90]3,[CSM]3 and [CSM, 0/90, CSM] although they had different tensile strength; the best laminate was [0/90]3 .

يهدف البحث الحالي الى دراسة تأثير نوع طبقات اللالياف الزجاجية على سلوك الكلال للمواد المتراكبه المصنعه من البولستر وبنسبه حجميه ثابتة للألياف الزجاجية مقدارها 33%. أظهرت نتائج البحث ان المواد المصنعه من ] [0/90, CSM, 0/90], [0/90,±45, 0/90 تمتلك أدنى حد للكلال عند 107 من تلك للمواد المصنعه من[0/90]3 و,[CSM, 0/90, CSM] [CSM]3 على الرغم من انها تمتلك اجهاد شد اقصى مختلف وان أفضل الطبقات هي[0/90]3.

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