Three-dimensional effects influencing failure in bend-free, variable stiffness composite pressure vessels

نویسندگان

چکیده

Abstract Pressure vessels enable liquids and gases to be stored transported safely, finding pervasive use in many industries. These types of structure can manufactured into different shapes from various materials satisfy the requirements their specific applications. Maximum allowable pressure is an important factor that should considered carefully design process. Bend-free vessels, are enabled by variable stiffness composite designs, even out in-plane stress distributions through-thickness direction thereby increasing overall load carrying capacity often accompanied significant weight reduction. therefore possible candidates for next generation it study failure performance, driven safety reasons. In this study, maximum internal determined bend-free ellipsoidal exploiting properties , using first-ply based on both Tsai-Wu recently proposed three-dimensional invariant-based criteria with performance subsequently compared against conventional constant stiffness, vessels. Parametric studies then performed provide physical insight also evaluate effect material difference prediction found these criteria.

برای دانلود رایگان متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Free vibration analysis of variable stiffness composite laminated thin skew plates using IGA

A NURBS-based isogeometric finite element formulation is developed and adopted to the free vibration analysis of finite square and skew laminated plates. Variable stiffness plies are assumed due to implementation of curvilinear fiberreinforcements. It is assumed due to employment of tow placement technology, in each ply of variable stiffness composite laminated plate the fiber reinforceme...

متن کامل

Free Vibration Analysis of Variable Stiffness Composite Laminates with Flat and Folded Shapes

In this article, free vibration analysis of variable stiffness composite laminate (VSCL) plates with flat and folded shapes is studied. In order to consider the concept of variable stiffness, in each layer of these composite laminated plates, the curvilinear fibers are used instead of straight fibers. The analysis is based on a semi-analytical finite strip method which follows classical laminat...

متن کامل

Three-dimensional anisotropic pressure free boundary equilibria

a r t i c l e i n f o a b s t r a c t Free boundary three-dimensional anisotropic pressure magnetohydrodynamic equilibria with nested magnetic flux surfaces are computed through the minimisation of the plasma energy functional W = V d 3 x [B 2 /(2μ 0) + p /(Γ − 1)]. The plasma–vacuum interface is varied to guarantee the continuity of the total pressure [p ⊥ + B 2 /(2μ 0)] across it and the vacu...

متن کامل

Free vibration analysisof soft-core composite-faced sandwich plates using three-dimensional finite element method

In this paper, natural frequencies of the sandwich plates with soft flexible core and composite face sheets are obtained. Three-Dimensional (3D) finite element method (FEM) is used for constructing and analyzing of the sandwich plates to obtain their natural frequencies. Continuity conditions for transverse shear stresses at the interfaces as well as transverse flexibility and transverse normal...

متن کامل

Three-dimensional 1-bend graph drawings

We consider three-dimensional grid-drawings of graphs with at most one bend per edge. Under the additional requirement that the vertices be collinear, we prove that the minimum volume of such a drawing is Θ(cn), where n is the number of vertices and c is the cutwidth of the graph. We then prove that every graph has a three-dimensional grid-drawing with O(n/ log n) volume and one bend per edge. ...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

ژورنال

عنوان ژورنال: Composite Structures

سال: 2021

ISSN: ['0263-8223', '1879-1085']

DOI: https://doi.org/10.1016/j.compstruct.2020.113346