“…A comprehensive study of the effect of the variation of the stiffness coefficients on the buckling behavior of filament-wound conical shells was performed by Goldfield and Arbocz [4]. Recently, Kayran and Yavuzbalkan [11] studied the effect of the variation of stiffness coefficients on the free-vibration characteristics of filament-wound shells by a semi-analytical method based on the numerical integration of the governing equations.…”
Section: Nomenclaturementioning
confidence: 99%
“…Solution of the natural frequencies is accomplished by evaluating the determinant of the characteristic matrix for incremented values of frequency estimates within a frequency range of interest. When the finite exponential Fourier transform of the fundamental shell equations was used, it was observed that determinant of the characteristic matrix does not change sign; rather, it is always positive and vanishes at the eigenvalue [11]. Therefore, a slope change detection algorithm in combination with inverse interpolations was devised to extract the natural frequency.…”
Section: Extension Of the Numerical Integration Technique To Branchedmentioning
confidence: 99%
“…Once an interval is determined, natural frequency is extracted by successive inverse interpolations. The details of the natural frequency extraction algorithm are described in [11]. It should be noted that extension of the multisegment numerical integration technique to the freevibration analysis of branched shells of revolution is simply accomplished by defining the transformation matrices TR at each junction j and modifying Eq.…”
Section: Extension Of the Numerical Integration Technique To Branchedmentioning
confidence: 99%
“…For a general shell of revolution with arbitrary change of geometric and material properties along the meridian of the shell, thickness, radii of curvature, and stiffness coefficients depend on the meridional coordinate . The elements of the coefficient matrix K for a general shell of revolution with full macroscopically anisotropic laminated shell wall are given in the recent work of Kayran and Yavuzbalkan [11], and they will not be repeated here, for brevity. Application of the finite exponential Fourier transform to Eq.…”
Application of the multisegment numerical integration technique is extended to the free-vibration analysis of macroscopically anisotropic filament-wound branched shells of revolution with ring stiffeners, considering the variation of the thickness and winding angle. The solution procedure is based on a modified-frequency trial method, which processes on the numerically integrated transformed fundamental shell equations that are obtained in terms of finite exponential Fourier transform of the fundamental shell variables. The full macroscopically anisotropic form of the constitutive relations, including first-order transverse shear deformation and all components of translatory and rotary inertia, are included in the analysis. To handle branched shells of revolution, modifications that are necessary to incorporate junctions are added to the solution procedure. Inclusion of asymmetric circumferential stiffeners, with respect to the middle surface of the shell, into the semi-analytical solution method is demonstrated by presenting two alternative methods of analysis. The present solution methodology also incorporates the variation of the thickness and winding angle along the meridian of filament-wound shells of revolution, with general meridional curvature, by assuming placement of filaments along the geodesic fiber path on the surface of the shell of revolution.
“…A comprehensive study of the effect of the variation of the stiffness coefficients on the buckling behavior of filament-wound conical shells was performed by Goldfield and Arbocz [4]. Recently, Kayran and Yavuzbalkan [11] studied the effect of the variation of stiffness coefficients on the free-vibration characteristics of filament-wound shells by a semi-analytical method based on the numerical integration of the governing equations.…”
Section: Nomenclaturementioning
confidence: 99%
“…Solution of the natural frequencies is accomplished by evaluating the determinant of the characteristic matrix for incremented values of frequency estimates within a frequency range of interest. When the finite exponential Fourier transform of the fundamental shell equations was used, it was observed that determinant of the characteristic matrix does not change sign; rather, it is always positive and vanishes at the eigenvalue [11]. Therefore, a slope change detection algorithm in combination with inverse interpolations was devised to extract the natural frequency.…”
Section: Extension Of the Numerical Integration Technique To Branchedmentioning
confidence: 99%
“…Once an interval is determined, natural frequency is extracted by successive inverse interpolations. The details of the natural frequency extraction algorithm are described in [11]. It should be noted that extension of the multisegment numerical integration technique to the freevibration analysis of branched shells of revolution is simply accomplished by defining the transformation matrices TR at each junction j and modifying Eq.…”
Section: Extension Of the Numerical Integration Technique To Branchedmentioning
confidence: 99%
“…For a general shell of revolution with arbitrary change of geometric and material properties along the meridian of the shell, thickness, radii of curvature, and stiffness coefficients depend on the meridional coordinate . The elements of the coefficient matrix K for a general shell of revolution with full macroscopically anisotropic laminated shell wall are given in the recent work of Kayran and Yavuzbalkan [11], and they will not be repeated here, for brevity. Application of the finite exponential Fourier transform to Eq.…”
Application of the multisegment numerical integration technique is extended to the free-vibration analysis of macroscopically anisotropic filament-wound branched shells of revolution with ring stiffeners, considering the variation of the thickness and winding angle. The solution procedure is based on a modified-frequency trial method, which processes on the numerically integrated transformed fundamental shell equations that are obtained in terms of finite exponential Fourier transform of the fundamental shell variables. The full macroscopically anisotropic form of the constitutive relations, including first-order transverse shear deformation and all components of translatory and rotary inertia, are included in the analysis. To handle branched shells of revolution, modifications that are necessary to incorporate junctions are added to the solution procedure. Inclusion of asymmetric circumferential stiffeners, with respect to the middle surface of the shell, into the semi-analytical solution method is demonstrated by presenting two alternative methods of analysis. The present solution methodology also incorporates the variation of the thickness and winding angle along the meridian of filament-wound shells of revolution, with general meridional curvature, by assuming placement of filaments along the geodesic fiber path on the surface of the shell of revolution.
“…Therefore, present study aims at presenting a comprehensive study of the effect of geodesic and semi-geodesic winding on the winding angle, stiffness and vibration characteristics of filament wound composite shells of revolution. The previous works of the authors 11,12 are extended by presenting additional results including the comparative study on the effect of taking constant winding angle and thickness versus using the actual variation of the winding angle and the thickness on the vibration characteristics. It should be noted that geodesic or semi-geodesic winding causes continuous meridional variation of the winding angle, thickness and the stiffness coefficients which also vary with the preset friction applied during the winding process.…”
Vibration characteristics of variable stiffness filament wound composite shells of revolution are investigated utilizing a numerical integration based solution method that is developed. Filaments are assumed to be placed along the geodesic and semi-geodesic fiber paths on the surface of the shell of revolution resulting in the variation of the stiffness coefficients and the thickness of the shell wall along the axis of the composite shell of revolution with general meridional curvature. For geodesic and semi-geodesic winding, relations giving the meridional variation of the winding angle and thickness are derived for truncated conical and spherical shells of revolution which are studied as the sample shell geometries. The effect of constant preset friction, applied during the winding process, on the stiffness and vibration characteristics of filament wound composite shells of revolution is studied in depth. In the most general case, multi-segment numerical integration technique is extended to the solution of the free vibration problem of composite shells of revolution which are wound along the semi-geodesic fiber paths counting on the preset friction used during the winding process. The effect of initial winding angle and the starting edge of the winding operation on the variation of the thickness, stiffness coefficients and free vibration characteristics of filament wound shells of revolution are investigated. Case studies are also performed on the comparison of the frequencies calculated by incorporating the actual variation of the winding angle and thickness, and the frequencies calculated based on constant winding angle and thickness which are taken as average and mid meridian values.
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