تلفن: ۰۴۱۴۲۲۷۳۷۸۱
تلفن: ۰۹۲۱۶۴۲۶۳۸۴

دانلود رایگان مقاله انگلیسی خصوصیات لرزش یک تیغه لمینیت کامپوزیت چرخشی قبل از پیچ خورده – الزویر ۲۰۱۹

عنوان فارسی: خصوصیات لرزش یک تیغه لمینیت کامپوزیت چرخشی قبل از پیچ خورده
عنوان انگلیسی: Vibration characteristics of a rotating pre-twisted composite laminated blade
تعداد صفحات مقاله انگلیسی : 13 تعداد صفحات ترجمه فارسی : ترجمه نشده
سال انتشار : 2019 نشریه : الزویر - Elsevier
فرمت مقاله انگلیسی : PDF نوع مقاله : ISI
نوع نگارش : مقالات پژوهشی (تحقیقاتی) پایگاه : اسکوپوس
کد محصول : E10808 رفرنس : دارد
محتوای فایل : PDF حجم فایل : mb 4
رشته های مرتبط با این مقاله: مهندسی عمران، مهندسی مواد
گرایش های مرتبط با این مقاله: زلزله، سازه، کامپوزیت
مجله: سازه های کامپوزیتی - Composite Structures
دانشگاه: Department of Architecture and Civil Engineering - City University of Hong Kong - China
کلمات کلیدی: چرخش پره پیچ خورده، ساختار لمینیت کامپوزیت، مشخصات ارتعاش، ارتعاش آزاد، تغییر جهت مکان فرکانس
doi یا شناسه دیجیتال: https://doi.org/10.1016/j.compstruct.2018.10.005
برای سفارش ترجمه این مقاله با کیفیت عالی و در کوتاه ترین زمان ممکن توسط مترجمین مجرب سایت ایران عرضه؛ روی دکمه سبز رنگ کلیک نمایید.
چکیده

ABSTRACT

A new dynamic model based on the shell theory is presented to investigate the vibration behavior of a rotating composite laminated blade with a pre-twisted angle. The effects of the Coriolis and centrifugal forces due to the rotation motion of the blade are considered in the formulation. Based on the Rayleigh-Ritz method and continuous algebraic polynomial functions satisfying the boundary conditions of a cantilever, the natural frequencies and mode shapes of a rotating pre-twisted blade are obtained. The convergence analysis is performed and the accuracy of the proposed model is verified by comparing the non-dimensional frequencies obtained by the present method with those in literature. The frequency loci veering and crossing phenomena along with the corresponding mode shape variations are presented and discussed in detail. A comprehensive parameter investigation of the effects of aspect ratio, pre-twisted angle, stagger angle, rotation velocity and hub radius on variations of the modal characteristics of the blade is conducted. It is demonstrated through the results of this paper that the developed model is effective to evaluate the dynamic behavior of rotating pre-twisted blades, which would be useful for improvement in design and optimization of the material and geometry dimension of the blades.

نتیجه گیری

Conclusion

In this paper, a dynamic model based on the shell theory was developed to investigate the vibration characteristics of a rotating composite laminated blade. The natural frequencies of a rotating pretwisted composite laminated blade were obtained by the Rayleigh-Ritz method. The convergence and comparison studies demonstrated the accuracy and validity of the present modeling method. The effects of the rotation velocity on the natural frequencies and the corresponding mode shapes of the blade were discussed. Due to the effects of the Coriolis and centrifugal forces, variation of different natural frequencies with rotation velocity was diverse, resulting in the phenomena of frequency loci veering and crossing. Two ways of frequency loci veer can be observed. For the first one, the nodal line patterns of the mode shapes switch their shapes to each other continuously. For the other one, the nodal line patterns vary in abrupt and discontinuously. A comprehensive parameter investigation of the effects of the aspect ratio, pre-twisted angle, stagger angle and hub radius on the variations of modal characteristics was conducted. Numerical results demonstrated that the natural frequencies of the rotating blade increase as the pre-twisted angle, stagger angle and the hub radius increase, while decrease as the thickness ratio increases. It was demonstrated through the results of this paper that the proposed model is an efficient tool for predicting the dynamic behavior of blades with arbitrary geometry dimension, stagger angle and pretwisted angle, which will provide useful information for the design and optimization of the blades. Based on the results of this paper, further investigations will extend to the internal resonances and nonlinear dynamics of the composite laminated blades rotating at high rotation velocity.