دانلود رایگان مقاله آکوستیک لانه زنبوری با افزایش سختی و مقاومت کمانش صفحه

عنوان فارسی
لانه زنبوری آکوستیک جدید با افزایش سختی و مقاومت کمانش صفحه
عنوان انگلیسی
A novel auxetic honeycomb with enhanced in-plane stiffness and buckling strength
صفحات مقاله فارسی
0
صفحات مقاله انگلیسی
12
سال انتشار
2016
نشریه
الزویر - Elsevier
فرمت مقاله انگلیسی
PDF
کد محصول
E507
رشته های مرتبط با این مقاله
مهندسی مکانیک و مهندسی مواد
گرایش های مرتبط با این مقاله
طراحی جامدات و متالوژی
مجله
ساختار کامپوزیت - Composite Structures
دانشگاه
گروه مکانیک کاربردی و مهندسی، دانشکده مهندسی، دانشگاه سون یات سن، چین
کلمات کلیدی
آکوستیک، داخل صفحه، خواص الاستیک، قدرت کمانش بحرانی
۰.۰ (بدون امتیاز)
امتیاز دهید
چکیده

Abstract


In the present work, a new design of honeycomb is proposed by embedding the rhombic configuration into the normal re-entrant hexagonal honeycomb (NRHH), in order to enhance the honeycomb’s in-plane mechanical properties. Both theoretical analysis and numerical simulations are employed to calculate the in-plane mechanical properties of the new honeycomb under uniaxial compression, including Young’s modulus, Poisson’s ratio and critical buckling strength. The results show that the new honeycomb can maintain auxetic performance, while both the in-plane Young’s modulus and the critical buckling strength are significantly improved compared to the NRHH. Comparisons between the present design and other exiting enhanced periodic topologies are also carried out. With respect to them, the present design features superior performances. For these outstanding properties, this layout may provide a new concept for the optimization and design of auxetic materials.

نتیجه گیری

5. Conclusion


Auxetic materials present a series of particular characteristics in comparison to conventional materials, such as enhancement of shear modulus, indentation resistance, and fracture toughness. However, the in-plane stiffness of them is relatively low. In this paper, a novel honeycomb, comprised of re-entrant hexagonal con- figuration and rhombic configuration, is developed. The new structure can be regarded as an optimization to the NRHH by embedding four reinforcing walls into every cell of it. The inplane effective modulus, i.e., the Young’s modulus and Poisson’s ratio, of the new honeycomb are analytically derived, which later verified by finite element simulations. Both the results obtained from the analytical and numerical analysis reveal that the new honeycomb can achieve negative Poisson’s ratio and the in-plane effective Young’s modulus of it is significantly improved compared to the NRHH. The dependence of the in-plane elastic constants on the reentrant angle h0, the cell wall length ratio h0=l0, normalized axial rigidity of the reinforcing walls ðE1A1Þ=ðE0A0Þ and the relative density q=q0 are further studied by using the numerically validated analytical solutions. With respect to the NRHH, the new proposed structure allows more geometric parameters in the unit cell, which provide enhanced in-plane flexibility and tailoring of properties. Results show that, for maintaining a superior auxetic performance, the reinforcing walls should be designed with appropriate axial rigidity. A comparison of in-plane stiffness is carried out between the present design and other periodic topologies. The results reveal that the new honeycomb developed in this paper shows superior stiffness and auxetic behavior with respect to the others.


بدون دیدگاه