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    Isogeometric analysis af laminated composite structures

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    ΠŸΡ€Π΅Π΄ΠΌΠ΅Ρ‚ ΠΎΠ²Π΅ докторскС Π΄ΠΈΡΠ΅Ρ€Ρ‚Π°Ρ†ΠΈΡ˜Π΅ јС Π°Π½Π°Π»ΠΈΠ·Π° Π»Π°ΠΌΠΈΠ½ΠΈΡ€Π°Π½ΠΈΡ… ΠΊΠΎΠΌΠΏΠΎΠ·ΠΈΡ‚Π½ΠΈΡ… структура ΡƒΠΏΠΎΡ‚Ρ€Π΅Π±ΠΎΠΌ ΠΈΠ·ΠΎΠ³Π΅ΠΎΠΌΠ΅Ρ‚Ρ€ΠΈΡ˜ΡΠΊΠΎΠ³ ΠΌΠ΅Ρ‚ΠΎΠ΄Π° ΠΊΠΎΠ½Π°Ρ‡Π½ΠΈΡ… Π΅Π»Π΅ΠΌΠ΅Π½Π°Ρ‚Π°. Π˜Π·ΠΎΠ³Π΅ΠΎΠΌΠ΅Ρ‚Ρ€ΠΈΡ˜ΡΠΊΠΈ ΠΌΠ΅Ρ‚ΠΎΠ΄ користи истС Π±Π°Π·Π½Π΅ Ρ„ΡƒΠ½ΠΊΡ†ΠΈΡ˜Π΅ Π·Π° Ρ€Π΅ΠΏΡ€Π΅Π·Π΅Π½Ρ‚Π°Ρ†ΠΈΡ˜Ρƒ Π³Π΅ΠΎΠΌΠ΅Ρ‚Ρ€ΠΈΡ˜Π΅ ΠΌΠΎΠ΄Π΅Π»Π° ΠΈ Π·Π° Π°ΠΏΡ€ΠΎΠΊΡΠΈΠΌΠ°Ρ†ΠΈΡ˜Ρƒ ΠΏΠΎΡ™Π° Π½Π΅ΠΏΠΎΠ·Π½Π°Ρ‚ΠΈΡ… Π²Π΅Π»ΠΈΡ‡ΠΈΠ½Π°. Π£ ΠΎΠΊΠ²ΠΈΡ€Ρƒ Π΄ΠΈΡΠ΅Ρ€Ρ‚Π°Ρ†ΠΈΡ˜Π΅ Ρ€Π°Π·Π²ΠΈΡ˜Π΅Π½ΠΈ су ΠΈΠ·ΠΎΠ³Π΅ΠΎΠΌΠ΅Ρ‚Ρ€ΠΈΡ˜ΡΠΊΠΈ ΠΌΠ°Ρ‚Π΅ΠΌΠ°Ρ‚ΠΈΡ‡ΠΊΠΈ ΠΌΠΎΠ΄Π΅Π»ΠΈ Π»Π°ΠΌΠΈΠ½ΠΈΡ€Π°Π½ΠΈΡ… ΠΏΠΎΠ²Ρ€ΡˆΠΈΠ½ΡΠΊΠΈΡ… носача формулисаних Π½Π° основу Ρ‚Π΅ΠΎΡ€ΠΈΡ˜Π° Π΅ΠΊΠ²ΠΈΠ²Π°Π»Π΅Π½Ρ‚Π½ΠΎΠ³ слоја Π±Π°Π·ΠΈΡ€Π°Π½ΠΈΡ… Π½Π° ΠšΠΈΡ€Ρ…ΠΎΡ„-Π›Π°Π²ΠΎΠ²ΠΎΡ˜, Миндлин-Π Π°Ρ˜Π·Π½Π΅Ρ€ΠΎΠ²ΠΎΡ˜ ΠΈ РСдијСвој Ρ‚Π΅ΠΎΡ€ΠΈΡ˜ΠΈ ΠΏΠΎΠ²Ρ€ΡˆΠΈΠ½ΡΠΊΠΈΡ… носача ΡƒΠ· ΡƒΠΏΠΎΡ‚Ρ€Π΅Π±Ρƒ NURBS Π±Π°Π·Π½ΠΈΡ… Ρ„ΡƒΠ½ΠΊΡ†ΠΈΡ˜Π°. Ѐормулисанe су основнС ΠΌΠ°Ρ‚Ρ€ΠΈΡ†Π΅ ΠΌΠ΅Ρ‚ΠΎΠ΄Π° ΠΊΠΎΠ½Π°Ρ‡Π½ΠΈΡ… Π΅Π»Π΅ΠΌΠ΅Π½Π°Ρ‚Π° Π·Π° статичку, Π΄ΠΈΠ½Π°ΠΌΠΈΡ‡ΠΊΡƒ ΠΈ Π°Π½Π°Π»ΠΈΠ·Ρƒ Π±ΠΈΡ„ΡƒΡ€ΠΊΠ°Ρ†ΠΈΠΎΠ½Π΅ стабилности Π·Π° свС Ρ‚Ρ€ΠΈ Ρ‚Π΅ΠΎΡ€ΠΈΡ˜Π΅ ΠΏΠΎΠ²Ρ€ΡˆΠΈΠ½ΡΠΊΠΈΡ… носача. Π’Π΅Π·Π΅ ΠΈΠ·ΠΌΠ΅Ρ’Ρƒ ΠΏΠΎΠΌΠ΅Ρ€Π°ΡšΠ° ΠΈ Π΄Π΅Ρ„ΠΎΡ€ΠΌΠ°Ρ†ΠΈΡ˜Π° су Π»ΠΈΠ½Π΅Π°Ρ€Π½Π΅, осим Ρƒ ΡΠ»ΡƒΡ‡Π°Ρ˜Ρƒ Π°Π½Π°Π»ΠΈΠ·Π΅ Π±ΠΈΡ„ΡƒΡ€ΠΊΠ°Ρ†ΠΈΠΎΠ½Π΅ стабилности Π³Π΄Π΅ јС ΠΊΠΎΡ€ΠΈΡˆΡ›Π΅Π½ стандардни Π½Π΅Π»ΠΈΠ½Π΅Π°Ρ€Π½ΠΈ ΠΌΠΎΠ΄Π΅Π» Π·Π° ΠΎΠ΄Ρ€Π΅Ρ’ΠΈΠ²Π°ΡšΠ΅ ΠΌΠ°Ρ‚Ρ€ΠΈΡ†Π΅ Π³Π΅ΠΎΠΌΠ΅Ρ‚Ρ€ΠΈΡ˜ΡΠΊΠ΅ крутости, Π΄ΠΎΠΊ јС Π²Π΅Π·Π° ΠΈΠ·ΠΌΠ΅Ρ’Ρƒ Π΄Π΅Ρ„ΠΎΡ€ΠΌΠ°Ρ†ΠΈΡ˜Π° ΠΈ Π½Π°ΠΏΠΎΠ½Π° Π»ΠΈΠ½Π΅Π°Ρ€Π½Π°. ОсновнС Ρ˜Π΅Π΄Π½Π°Ρ‡ΠΈΠ½Π΅ ΠΌΠ΅Ρ‚ΠΎΠ΄Π° ΠΊΠΎΠ½Π°Ρ‡Π½ΠΈΡ… Π΅Π»Π΅ΠΌΠ΅Π½Π°Ρ‚Π° ΠΈΠ·Π²Π΅Π΄Π΅Π½Π΅ су ΠΌΠ΅Ρ‚ΠΎΠ΄ΠΎΠΌ ΠΏΠΎΠΌΠ΅Ρ€Π°Ρ˜Π°. Π£ ΠΎΠΊΠ²ΠΈΡ€Ρƒ Π΄ΠΈΡΠ΅Ρ€Ρ‚Π°Ρ†ΠΈΡ˜Π΅ ΠΈΠ·Π²Ρ€ΡˆΠ΅Π½ΠΎ јС опсСТно Π½ΡƒΠΌΠ΅Ρ€ΠΈΡ‡ΠΊΠΎ Ρ‚Π΅ΡΡ‚ΠΈΡ€Π°ΡšΠ΅ ΠΏΡ€Π΅Π΄Π»ΠΎΠΆΠ΅Π½ΠΈΡ… ΠΌΠ΅Ρ‚ΠΎΠ΄Π° ΠΈ добијСни Ρ€Π΅Π·ΡƒΠ»Ρ‚Π°Ρ‚ΠΈ су ΡƒΠΏΠΎΡ€Π΅Ρ’Π΅Π½ΠΈ са Π°Π½Π°Π»ΠΈΡ‚ΠΈΡ‡ΠΊΠΈΠΌ Ρ€Π΅ΡˆΠ΅ΡšΠΈΠΌΠ° ΠΈ осталим доступним Ρ€Π΅Π·ΡƒΠ»Ρ‚Π°Ρ‚ΠΈΠΌΠ°. Π”ΠΎΠΊΠ°Π·Π°Π½Π° јС Π²Π΅Π»ΠΈΠΊΠ° тачност ΠΌΠ΅Ρ‚ΠΎΠ΄Π° Ρƒ односу Π½Π° ΠΊΠΎΠ½Π²Π΅Π½Ρ†ΠΈΠΎΠ½Π°Π»Π½ΠΈ ΠΌΠ΅Ρ‚ΠΎΠ΄ ΠΊΠΎΠ½Π°Ρ‡Π½ΠΈΡ… Π΅Π»Π΅ΠΌΠ΅Π½Π°Ρ‚Π° ΠΈ ΠΏΠΎΡΡ‚ΠΎΡ˜Π΅Ρ›Π΅ Π°Π»Ρ‚Π΅Ρ€Π½Π°Ρ‚ΠΈΠ²Π½Π΅ ΠΌΠ΅Ρ‚ΠΎΠ΄Π΅. Π‘Ρ‚Π°Ρ‚ΠΈΡ‡ΠΊΠ° Π°Π½Π°Π»ΠΈΠ·Π° ΠΌΠΎΠ΄Π΅Π»Π° ΠΏΠΎΠΊΠ°Π·Π°Π»Π° јС високу тачност ΠΌΠ΅Ρ‚ΠΎΠ΄Π° ΠΈ прСдности ΡƒΠΏΠΎΡ‚Ρ€Π΅Π±Π΅ Π±Π°Π·Π½ΠΈΡ… Ρ„ΡƒΠ½ΠΊΡ†ΠΈΡ˜Π° вишСг Ρ€Π΅Π΄Π°. ΠšΠΎΡ€ΠΈΡΡ‚Π΅Ρ›ΠΈ особинС NURBS Π±Π°Π·Π½ΠΈΡ… Ρ„ΡƒΠ½ΠΊΡ†ΠΈΡ˜Π° Ρ€Π°Π·Π²ΠΈΡ˜Π΅Π½Π° јС ΠΌΠ΅Ρ‚ΠΎΠ΄ΠΎΠ»ΠΎΠ³ΠΈΡ˜Π° ΠΏΡ€ΠΎΡ€Π°Ρ‡ΡƒΠ½Π° ΠΈΠ½Ρ‚Π΅Ρ€Π»Π°ΠΌΠΈΠ½Π°Ρ€Π½ΠΈΡ… Π½Π°ΠΏΠΎΠ½Π° Ρƒ засСбном ΠΊΠΎΡ€Π°ΠΊΡƒ, Π½Π°ΠΊΠΎΠ½ ΠΈΠ·Ρ€Π°Ρ‡ΡƒΠ½Π°Π²Π°ΡšΠ° ΠΏΠΎΡ™Π° ΠΏΠΎΠΌΠ΅Ρ€Π°ΡšΠ°. Π˜Π·Ρ€Π°Ρ‡ΡƒΠ½Π°Ρ‚ΠΈ су ΠΈΠ½Ρ‚Π΅Ρ€Π»Π°ΠΌΠΈΠ½Π°Ρ€Π½ΠΈ Π½Π°ΠΏΠΎΠ½ΠΈ ΠΊΠΎΡ€ΠΈΡˆΡ›Π΅ΡšΠ΅ΠΌ Ρ˜Π΅Π΄Π½Π°Ρ‡ΠΈΠ½Π° Ρ€Π°Π²Π½ΠΎΡ‚Π΅ΠΆΠ΅ Π·Π° ΠΏΠ»ΠΎΡ‡Π΅ ΠΌΠΎΠ΄Π΅Π»ΠΎΠ²Π°Π½Π΅ Ρ€Π°Π·Π»ΠΈΡ‡ΠΈΡ‚ΠΈΠΌ Ρ‚Π΅ΠΎΡ€ΠΈΡ˜Π°ΠΌΠ° ΠΏΠΎΠ²Ρ€ΡˆΠΈΠ½ΡΠΊΠΈΡ… носача ΠΈ ΠΏΠΎΠΊΠ°Π·Π°Π½Π° јС ΡšΠΈΡ…ΠΎΠ²Π° Π²Π΅Π»ΠΈΠΊΠ° тачност Ρƒ односу Π½Π° ΠΈΠ½Ρ‚Π΅Ρ€Π»Π°ΠΌΠΈΠ½Π°Ρ€Π½Π΅ Π½Π°ΠΏΠΎΠ½Π΅ добијСнС ΠΈΠ· конститутивних Ρ˜Π΅Π΄Π½Π°Ρ‡ΠΈΠ½Π°. Анализа слободних Π²ΠΈΠ±Ρ€Π°Ρ†ΠΈΡ˜Π° ΠΈ Π±ΠΈΡ„ΡƒΡ€ΠΊΠ°Ρ†ΠΈΠΎΠ½Π΅ стабилности ΠΏΠΎΠΊΠ°Π·Π°Π»Π΅ су високу тачност ΠΌΠ΅Ρ‚ΠΎΠ΄Π°...This doctoral dissertation deals with analysis of laminated composite structures using isogeometric finite element method. In isogeometric analysis same basis functions that are used for geometry representation are also used for approximation of unknown quantities. Isogeometrical mathematical models of laminated thin walled structures are formulated. The proposed models are based on most popular equivalent layer theories, that is Kirchoff-love, Mindlin-Reissner and Reddy's plate theories with the use of NURBS basis functions. Main matrices of finite element method for static, dynamic and stability analysis are formulated for all three plate theories. Relation between displacements and strains are linear, except for the case of stability analysis where standard non-linear procedure is used for geometric stiffness matrix formulation. Constitutive relations are linear. Finite element equations are derived using displacement method, Extensive numerical testing of the proposed method is conducted in order to verify the performance of the method. Obtained results are compared with analytical solutions and other available results. The obtained results demonstrated high accuracy of the method in comparison to the conventional finite element method and existing alternatives. Static analysis of developed models showed high accuracy of the proposed formulation and the advantages of using higher-order basis functions. Using the properties of NURBS basis functions, methodology for interlaminar stress calculation is developed that is able to accurately compute interlaminar stresses in a single separate step, after calculation of displacement field is performed. The interlaminar stresses are calculated using the equilibrium equations for plates modeled with different plate theories. High accuracy of equilibrium interlaminar stresses compared to constitutive interlaminar stresses is demonstrated. Free vibration and buckling analysis also demonstrated high accuracy of the method..

    Isogeometric analysis af laminated composite structures

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    ΠŸΡ€Π΅Π΄ΠΌΠ΅Ρ‚ ΠΎΠ²Π΅ докторскС Π΄ΠΈΡΠ΅Ρ€Ρ‚Π°Ρ†ΠΈΡ˜Π΅ јС Π°Π½Π°Π»ΠΈΠ·Π° Π»Π°ΠΌΠΈΠ½ΠΈΡ€Π°Π½ΠΈΡ… ΠΊΠΎΠΌΠΏΠΎΠ·ΠΈΡ‚Π½ΠΈΡ… структура ΡƒΠΏΠΎΡ‚Ρ€Π΅Π±ΠΎΠΌ ΠΈΠ·ΠΎΠ³Π΅ΠΎΠΌΠ΅Ρ‚Ρ€ΠΈΡ˜ΡΠΊΠΎΠ³ ΠΌΠ΅Ρ‚ΠΎΠ΄Π° ΠΊΠΎΠ½Π°Ρ‡Π½ΠΈΡ… Π΅Π»Π΅ΠΌΠ΅Π½Π°Ρ‚Π°. Π˜Π·ΠΎΠ³Π΅ΠΎΠΌΠ΅Ρ‚Ρ€ΠΈΡ˜ΡΠΊΠΈ ΠΌΠ΅Ρ‚ΠΎΠ΄ користи истС Π±Π°Π·Π½Π΅ Ρ„ΡƒΠ½ΠΊΡ†ΠΈΡ˜Π΅ Π·Π° Ρ€Π΅ΠΏΡ€Π΅Π·Π΅Π½Ρ‚Π°Ρ†ΠΈΡ˜Ρƒ Π³Π΅ΠΎΠΌΠ΅Ρ‚Ρ€ΠΈΡ˜Π΅ ΠΌΠΎΠ΄Π΅Π»Π° ΠΈ Π·Π° Π°ΠΏΡ€ΠΎΠΊΡΠΈΠΌΠ°Ρ†ΠΈΡ˜Ρƒ ΠΏΠΎΡ™Π° Π½Π΅ΠΏΠΎΠ·Π½Π°Ρ‚ΠΈΡ… Π²Π΅Π»ΠΈΡ‡ΠΈΠ½Π°. Π£ ΠΎΠΊΠ²ΠΈΡ€Ρƒ Π΄ΠΈΡΠ΅Ρ€Ρ‚Π°Ρ†ΠΈΡ˜Π΅ Ρ€Π°Π·Π²ΠΈΡ˜Π΅Π½ΠΈ су ΠΈΠ·ΠΎΠ³Π΅ΠΎΠΌΠ΅Ρ‚Ρ€ΠΈΡ˜ΡΠΊΠΈ ΠΌΠ°Ρ‚Π΅ΠΌΠ°Ρ‚ΠΈΡ‡ΠΊΠΈ ΠΌΠΎΠ΄Π΅Π»ΠΈ Π»Π°ΠΌΠΈΠ½ΠΈΡ€Π°Π½ΠΈΡ… ΠΏΠΎΠ²Ρ€ΡˆΠΈΠ½ΡΠΊΠΈΡ… носача формулисаних Π½Π° основу Ρ‚Π΅ΠΎΡ€ΠΈΡ˜Π° Π΅ΠΊΠ²ΠΈΠ²Π°Π»Π΅Π½Ρ‚Π½ΠΎΠ³ слоја Π±Π°Π·ΠΈΡ€Π°Π½ΠΈΡ… Π½Π° ΠšΠΈΡ€Ρ…ΠΎΡ„-Π›Π°Π²ΠΎΠ²ΠΎΡ˜, Миндлин-Π Π°Ρ˜Π·Π½Π΅Ρ€ΠΎΠ²ΠΎΡ˜ ΠΈ РСдијСвој Ρ‚Π΅ΠΎΡ€ΠΈΡ˜ΠΈ ΠΏΠΎΠ²Ρ€ΡˆΠΈΠ½ΡΠΊΠΈΡ… носача ΡƒΠ· ΡƒΠΏΠΎΡ‚Ρ€Π΅Π±Ρƒ NURBS Π±Π°Π·Π½ΠΈΡ… Ρ„ΡƒΠ½ΠΊΡ†ΠΈΡ˜Π°. Ѐормулисанe су основнС ΠΌΠ°Ρ‚Ρ€ΠΈΡ†Π΅ ΠΌΠ΅Ρ‚ΠΎΠ΄Π° ΠΊΠΎΠ½Π°Ρ‡Π½ΠΈΡ… Π΅Π»Π΅ΠΌΠ΅Π½Π°Ρ‚Π° Π·Π° статичку, Π΄ΠΈΠ½Π°ΠΌΠΈΡ‡ΠΊΡƒ ΠΈ Π°Π½Π°Π»ΠΈΠ·Ρƒ Π±ΠΈΡ„ΡƒΡ€ΠΊΠ°Ρ†ΠΈΠΎΠ½Π΅ стабилности Π·Π° свС Ρ‚Ρ€ΠΈ Ρ‚Π΅ΠΎΡ€ΠΈΡ˜Π΅ ΠΏΠΎΠ²Ρ€ΡˆΠΈΠ½ΡΠΊΠΈΡ… носача. Π’Π΅Π·Π΅ ΠΈΠ·ΠΌΠ΅Ρ’Ρƒ ΠΏΠΎΠΌΠ΅Ρ€Π°ΡšΠ° ΠΈ Π΄Π΅Ρ„ΠΎΡ€ΠΌΠ°Ρ†ΠΈΡ˜Π° су Π»ΠΈΠ½Π΅Π°Ρ€Π½Π΅, осим Ρƒ ΡΠ»ΡƒΡ‡Π°Ρ˜Ρƒ Π°Π½Π°Π»ΠΈΠ·Π΅ Π±ΠΈΡ„ΡƒΡ€ΠΊΠ°Ρ†ΠΈΠΎΠ½Π΅ стабилности Π³Π΄Π΅ јС ΠΊΠΎΡ€ΠΈΡˆΡ›Π΅Π½ стандардни Π½Π΅Π»ΠΈΠ½Π΅Π°Ρ€Π½ΠΈ ΠΌΠΎΠ΄Π΅Π» Π·Π° ΠΎΠ΄Ρ€Π΅Ρ’ΠΈΠ²Π°ΡšΠ΅ ΠΌΠ°Ρ‚Ρ€ΠΈΡ†Π΅ Π³Π΅ΠΎΠΌΠ΅Ρ‚Ρ€ΠΈΡ˜ΡΠΊΠ΅ крутости, Π΄ΠΎΠΊ јС Π²Π΅Π·Π° ΠΈΠ·ΠΌΠ΅Ρ’Ρƒ Π΄Π΅Ρ„ΠΎΡ€ΠΌΠ°Ρ†ΠΈΡ˜Π° ΠΈ Π½Π°ΠΏΠΎΠ½Π° Π»ΠΈΠ½Π΅Π°Ρ€Π½Π°. ОсновнС Ρ˜Π΅Π΄Π½Π°Ρ‡ΠΈΠ½Π΅ ΠΌΠ΅Ρ‚ΠΎΠ΄Π° ΠΊΠΎΠ½Π°Ρ‡Π½ΠΈΡ… Π΅Π»Π΅ΠΌΠ΅Π½Π°Ρ‚Π° ΠΈΠ·Π²Π΅Π΄Π΅Π½Π΅ су ΠΌΠ΅Ρ‚ΠΎΠ΄ΠΎΠΌ ΠΏΠΎΠΌΠ΅Ρ€Π°Ρ˜Π°. Π£ ΠΎΠΊΠ²ΠΈΡ€Ρƒ Π΄ΠΈΡΠ΅Ρ€Ρ‚Π°Ρ†ΠΈΡ˜Π΅ ΠΈΠ·Π²Ρ€ΡˆΠ΅Π½ΠΎ јС опсСТно Π½ΡƒΠΌΠ΅Ρ€ΠΈΡ‡ΠΊΠΎ Ρ‚Π΅ΡΡ‚ΠΈΡ€Π°ΡšΠ΅ ΠΏΡ€Π΅Π΄Π»ΠΎΠΆΠ΅Π½ΠΈΡ… ΠΌΠ΅Ρ‚ΠΎΠ΄Π° ΠΈ добијСни Ρ€Π΅Π·ΡƒΠ»Ρ‚Π°Ρ‚ΠΈ су ΡƒΠΏΠΎΡ€Π΅Ρ’Π΅Π½ΠΈ са Π°Π½Π°Π»ΠΈΡ‚ΠΈΡ‡ΠΊΠΈΠΌ Ρ€Π΅ΡˆΠ΅ΡšΠΈΠΌΠ° ΠΈ осталим доступним Ρ€Π΅Π·ΡƒΠ»Ρ‚Π°Ρ‚ΠΈΠΌΠ°. Π”ΠΎΠΊΠ°Π·Π°Π½Π° јС Π²Π΅Π»ΠΈΠΊΠ° тачност ΠΌΠ΅Ρ‚ΠΎΠ΄Π° Ρƒ односу Π½Π° ΠΊΠΎΠ½Π²Π΅Π½Ρ†ΠΈΠΎΠ½Π°Π»Π½ΠΈ ΠΌΠ΅Ρ‚ΠΎΠ΄ ΠΊΠΎΠ½Π°Ρ‡Π½ΠΈΡ… Π΅Π»Π΅ΠΌΠ΅Π½Π°Ρ‚Π° ΠΈ ΠΏΠΎΡΡ‚ΠΎΡ˜Π΅Ρ›Π΅ Π°Π»Ρ‚Π΅Ρ€Π½Π°Ρ‚ΠΈΠ²Π½Π΅ ΠΌΠ΅Ρ‚ΠΎΠ΄Π΅. Π‘Ρ‚Π°Ρ‚ΠΈΡ‡ΠΊΠ° Π°Π½Π°Π»ΠΈΠ·Π° ΠΌΠΎΠ΄Π΅Π»Π° ΠΏΠΎΠΊΠ°Π·Π°Π»Π° јС високу тачност ΠΌΠ΅Ρ‚ΠΎΠ΄Π° ΠΈ прСдности ΡƒΠΏΠΎΡ‚Ρ€Π΅Π±Π΅ Π±Π°Π·Π½ΠΈΡ… Ρ„ΡƒΠ½ΠΊΡ†ΠΈΡ˜Π° вишСг Ρ€Π΅Π΄Π°. ΠšΠΎΡ€ΠΈΡΡ‚Π΅Ρ›ΠΈ особинС NURBS Π±Π°Π·Π½ΠΈΡ… Ρ„ΡƒΠ½ΠΊΡ†ΠΈΡ˜Π° Ρ€Π°Π·Π²ΠΈΡ˜Π΅Π½Π° јС ΠΌΠ΅Ρ‚ΠΎΠ΄ΠΎΠ»ΠΎΠ³ΠΈΡ˜Π° ΠΏΡ€ΠΎΡ€Π°Ρ‡ΡƒΠ½Π° ΠΈΠ½Ρ‚Π΅Ρ€Π»Π°ΠΌΠΈΠ½Π°Ρ€Π½ΠΈΡ… Π½Π°ΠΏΠΎΠ½Π° Ρƒ засСбном ΠΊΠΎΡ€Π°ΠΊΡƒ, Π½Π°ΠΊΠΎΠ½ ΠΈΠ·Ρ€Π°Ρ‡ΡƒΠ½Π°Π²Π°ΡšΠ° ΠΏΠΎΡ™Π° ΠΏΠΎΠΌΠ΅Ρ€Π°ΡšΠ°. Π˜Π·Ρ€Π°Ρ‡ΡƒΠ½Π°Ρ‚ΠΈ су ΠΈΠ½Ρ‚Π΅Ρ€Π»Π°ΠΌΠΈΠ½Π°Ρ€Π½ΠΈ Π½Π°ΠΏΠΎΠ½ΠΈ ΠΊΠΎΡ€ΠΈΡˆΡ›Π΅ΡšΠ΅ΠΌ Ρ˜Π΅Π΄Π½Π°Ρ‡ΠΈΠ½Π° Ρ€Π°Π²Π½ΠΎΡ‚Π΅ΠΆΠ΅ Π·Π° ΠΏΠ»ΠΎΡ‡Π΅ ΠΌΠΎΠ΄Π΅Π»ΠΎΠ²Π°Π½Π΅ Ρ€Π°Π·Π»ΠΈΡ‡ΠΈΡ‚ΠΈΠΌ Ρ‚Π΅ΠΎΡ€ΠΈΡ˜Π°ΠΌΠ° ΠΏΠΎΠ²Ρ€ΡˆΠΈΠ½ΡΠΊΠΈΡ… носача ΠΈ ΠΏΠΎΠΊΠ°Π·Π°Π½Π° јС ΡšΠΈΡ…ΠΎΠ²Π° Π²Π΅Π»ΠΈΠΊΠ° тачност Ρƒ односу Π½Π° ΠΈΠ½Ρ‚Π΅Ρ€Π»Π°ΠΌΠΈΠ½Π°Ρ€Π½Π΅ Π½Π°ΠΏΠΎΠ½Π΅ добијСнС ΠΈΠ· конститутивних Ρ˜Π΅Π΄Π½Π°Ρ‡ΠΈΠ½Π°. Анализа слободних Π²ΠΈΠ±Ρ€Π°Ρ†ΠΈΡ˜Π° ΠΈ Π±ΠΈΡ„ΡƒΡ€ΠΊΠ°Ρ†ΠΈΠΎΠ½Π΅ стабилности ΠΏΠΎΠΊΠ°Π·Π°Π»Π΅ су високу тачност ΠΌΠ΅Ρ‚ΠΎΠ΄Π°...This doctoral dissertation deals with analysis of laminated composite structures using isogeometric finite element method. In isogeometric analysis same basis functions that are used for geometry representation are also used for approximation of unknown quantities. Isogeometrical mathematical models of laminated thin walled structures are formulated. The proposed models are based on most popular equivalent layer theories, that is Kirchoff-love, Mindlin-Reissner and Reddy's plate theories with the use of NURBS basis functions. Main matrices of finite element method for static, dynamic and stability analysis are formulated for all three plate theories. Relation between displacements and strains are linear, except for the case of stability analysis where standard non-linear procedure is used for geometric stiffness matrix formulation. Constitutive relations are linear. Finite element equations are derived using displacement method, Extensive numerical testing of the proposed method is conducted in order to verify the performance of the method. Obtained results are compared with analytical solutions and other available results. The obtained results demonstrated high accuracy of the method in comparison to the conventional finite element method and existing alternatives. Static analysis of developed models showed high accuracy of the proposed formulation and the advantages of using higher-order basis functions. Using the properties of NURBS basis functions, methodology for interlaminar stress calculation is developed that is able to accurately compute interlaminar stresses in a single separate step, after calculation of displacement field is performed. The interlaminar stresses are calculated using the equilibrium equations for plates modeled with different plate theories. High accuracy of equilibrium interlaminar stresses compared to constitutive interlaminar stresses is demonstrated. Free vibration and buckling analysis also demonstrated high accuracy of the method..

    Isogeometric analysis af laminated composite structures

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    ΠŸΡ€Π΅Π΄ΠΌΠ΅Ρ‚ ΠΎΠ²Π΅ докторскС Π΄ΠΈΡΠ΅Ρ€Ρ‚Π°Ρ†ΠΈΡ˜Π΅ јС Π°Π½Π°Π»ΠΈΠ·Π° Π»Π°ΠΌΠΈΠ½ΠΈΡ€Π°Π½ΠΈΡ… ΠΊΠΎΠΌΠΏΠΎΠ·ΠΈΡ‚Π½ΠΈΡ… структура ΡƒΠΏΠΎΡ‚Ρ€Π΅Π±ΠΎΠΌ ΠΈΠ·ΠΎΠ³Π΅ΠΎΠΌΠ΅Ρ‚Ρ€ΠΈΡ˜ΡΠΊΠΎΠ³ ΠΌΠ΅Ρ‚ΠΎΠ΄Π° ΠΊΠΎΠ½Π°Ρ‡Π½ΠΈΡ… Π΅Π»Π΅ΠΌΠ΅Π½Π°Ρ‚Π°. Π˜Π·ΠΎΠ³Π΅ΠΎΠΌΠ΅Ρ‚Ρ€ΠΈΡ˜ΡΠΊΠΈ ΠΌΠ΅Ρ‚ΠΎΠ΄ користи истС Π±Π°Π·Π½Π΅ Ρ„ΡƒΠ½ΠΊΡ†ΠΈΡ˜Π΅ Π·Π° Ρ€Π΅ΠΏΡ€Π΅Π·Π΅Π½Ρ‚Π°Ρ†ΠΈΡ˜Ρƒ Π³Π΅ΠΎΠΌΠ΅Ρ‚Ρ€ΠΈΡ˜Π΅ ΠΌΠΎΠ΄Π΅Π»Π° ΠΈ Π·Π° Π°ΠΏΡ€ΠΎΠΊΡΠΈΠΌΠ°Ρ†ΠΈΡ˜Ρƒ ΠΏΠΎΡ™Π° Π½Π΅ΠΏΠΎΠ·Π½Π°Ρ‚ΠΈΡ… Π²Π΅Π»ΠΈΡ‡ΠΈΠ½Π°. Π£ ΠΎΠΊΠ²ΠΈΡ€Ρƒ Π΄ΠΈΡΠ΅Ρ€Ρ‚Π°Ρ†ΠΈΡ˜Π΅ Ρ€Π°Π·Π²ΠΈΡ˜Π΅Π½ΠΈ су ΠΈΠ·ΠΎΠ³Π΅ΠΎΠΌΠ΅Ρ‚Ρ€ΠΈΡ˜ΡΠΊΠΈ ΠΌΠ°Ρ‚Π΅ΠΌΠ°Ρ‚ΠΈΡ‡ΠΊΠΈ ΠΌΠΎΠ΄Π΅Π»ΠΈ Π»Π°ΠΌΠΈΠ½ΠΈΡ€Π°Π½ΠΈΡ… ΠΏΠΎΠ²Ρ€ΡˆΠΈΠ½ΡΠΊΠΈΡ… носача формулисаних Π½Π° основу Ρ‚Π΅ΠΎΡ€ΠΈΡ˜Π° Π΅ΠΊΠ²ΠΈΠ²Π°Π»Π΅Π½Ρ‚Π½ΠΎΠ³ слоја Π±Π°Π·ΠΈΡ€Π°Π½ΠΈΡ… Π½Π° ΠšΠΈΡ€Ρ…ΠΎΡ„-Π›Π°Π²ΠΎΠ²ΠΎΡ˜, Миндлин-Π Π°Ρ˜Π·Π½Π΅Ρ€ΠΎΠ²ΠΎΡ˜ ΠΈ РСдијСвој Ρ‚Π΅ΠΎΡ€ΠΈΡ˜ΠΈ ΠΏΠΎΠ²Ρ€ΡˆΠΈΠ½ΡΠΊΠΈΡ… носача ΡƒΠ· ΡƒΠΏΠΎΡ‚Ρ€Π΅Π±Ρƒ NURBS Π±Π°Π·Π½ΠΈΡ… Ρ„ΡƒΠ½ΠΊΡ†ΠΈΡ˜Π°. Ѐормулисанe су основнС ΠΌΠ°Ρ‚Ρ€ΠΈΡ†Π΅ ΠΌΠ΅Ρ‚ΠΎΠ΄Π° ΠΊΠΎΠ½Π°Ρ‡Π½ΠΈΡ… Π΅Π»Π΅ΠΌΠ΅Π½Π°Ρ‚Π° Π·Π° статичку, Π΄ΠΈΠ½Π°ΠΌΠΈΡ‡ΠΊΡƒ ΠΈ Π°Π½Π°Π»ΠΈΠ·Ρƒ Π±ΠΈΡ„ΡƒΡ€ΠΊΠ°Ρ†ΠΈΠΎΠ½Π΅ стабилности Π·Π° свС Ρ‚Ρ€ΠΈ Ρ‚Π΅ΠΎΡ€ΠΈΡ˜Π΅ ΠΏΠΎΠ²Ρ€ΡˆΠΈΠ½ΡΠΊΠΈΡ… носача. Π’Π΅Π·Π΅ ΠΈΠ·ΠΌΠ΅Ρ’Ρƒ ΠΏΠΎΠΌΠ΅Ρ€Π°ΡšΠ° ΠΈ Π΄Π΅Ρ„ΠΎΡ€ΠΌΠ°Ρ†ΠΈΡ˜Π° су Π»ΠΈΠ½Π΅Π°Ρ€Π½Π΅, осим Ρƒ ΡΠ»ΡƒΡ‡Π°Ρ˜Ρƒ Π°Π½Π°Π»ΠΈΠ·Π΅ Π±ΠΈΡ„ΡƒΡ€ΠΊΠ°Ρ†ΠΈΠΎΠ½Π΅ стабилности Π³Π΄Π΅ јС ΠΊΠΎΡ€ΠΈΡˆΡ›Π΅Π½ стандардни Π½Π΅Π»ΠΈΠ½Π΅Π°Ρ€Π½ΠΈ ΠΌΠΎΠ΄Π΅Π» Π·Π° ΠΎΠ΄Ρ€Π΅Ρ’ΠΈΠ²Π°ΡšΠ΅ ΠΌΠ°Ρ‚Ρ€ΠΈΡ†Π΅ Π³Π΅ΠΎΠΌΠ΅Ρ‚Ρ€ΠΈΡ˜ΡΠΊΠ΅ крутости, Π΄ΠΎΠΊ јС Π²Π΅Π·Π° ΠΈΠ·ΠΌΠ΅Ρ’Ρƒ Π΄Π΅Ρ„ΠΎΡ€ΠΌΠ°Ρ†ΠΈΡ˜Π° ΠΈ Π½Π°ΠΏΠΎΠ½Π° Π»ΠΈΠ½Π΅Π°Ρ€Π½Π°. ОсновнС Ρ˜Π΅Π΄Π½Π°Ρ‡ΠΈΠ½Π΅ ΠΌΠ΅Ρ‚ΠΎΠ΄Π° ΠΊΠΎΠ½Π°Ρ‡Π½ΠΈΡ… Π΅Π»Π΅ΠΌΠ΅Π½Π°Ρ‚Π° ΠΈΠ·Π²Π΅Π΄Π΅Π½Π΅ су ΠΌΠ΅Ρ‚ΠΎΠ΄ΠΎΠΌ ΠΏΠΎΠΌΠ΅Ρ€Π°Ρ˜Π°. Π£ ΠΎΠΊΠ²ΠΈΡ€Ρƒ Π΄ΠΈΡΠ΅Ρ€Ρ‚Π°Ρ†ΠΈΡ˜Π΅ ΠΈΠ·Π²Ρ€ΡˆΠ΅Π½ΠΎ јС опсСТно Π½ΡƒΠΌΠ΅Ρ€ΠΈΡ‡ΠΊΠΎ Ρ‚Π΅ΡΡ‚ΠΈΡ€Π°ΡšΠ΅ ΠΏΡ€Π΅Π΄Π»ΠΎΠΆΠ΅Π½ΠΈΡ… ΠΌΠ΅Ρ‚ΠΎΠ΄Π° ΠΈ добијСни Ρ€Π΅Π·ΡƒΠ»Ρ‚Π°Ρ‚ΠΈ су ΡƒΠΏΠΎΡ€Π΅Ρ’Π΅Π½ΠΈ са Π°Π½Π°Π»ΠΈΡ‚ΠΈΡ‡ΠΊΠΈΠΌ Ρ€Π΅ΡˆΠ΅ΡšΠΈΠΌΠ° ΠΈ осталим доступним Ρ€Π΅Π·ΡƒΠ»Ρ‚Π°Ρ‚ΠΈΠΌΠ°. Π”ΠΎΠΊΠ°Π·Π°Π½Π° јС Π²Π΅Π»ΠΈΠΊΠ° тачност ΠΌΠ΅Ρ‚ΠΎΠ΄Π° Ρƒ односу Π½Π° ΠΊΠΎΠ½Π²Π΅Π½Ρ†ΠΈΠΎΠ½Π°Π»Π½ΠΈ ΠΌΠ΅Ρ‚ΠΎΠ΄ ΠΊΠΎΠ½Π°Ρ‡Π½ΠΈΡ… Π΅Π»Π΅ΠΌΠ΅Π½Π°Ρ‚Π° ΠΈ ΠΏΠΎΡΡ‚ΠΎΡ˜Π΅Ρ›Π΅ Π°Π»Ρ‚Π΅Ρ€Π½Π°Ρ‚ΠΈΠ²Π½Π΅ ΠΌΠ΅Ρ‚ΠΎΠ΄Π΅. Π‘Ρ‚Π°Ρ‚ΠΈΡ‡ΠΊΠ° Π°Π½Π°Π»ΠΈΠ·Π° ΠΌΠΎΠ΄Π΅Π»Π° ΠΏΠΎΠΊΠ°Π·Π°Π»Π° јС високу тачност ΠΌΠ΅Ρ‚ΠΎΠ΄Π° ΠΈ прСдности ΡƒΠΏΠΎΡ‚Ρ€Π΅Π±Π΅ Π±Π°Π·Π½ΠΈΡ… Ρ„ΡƒΠ½ΠΊΡ†ΠΈΡ˜Π° вишСг Ρ€Π΅Π΄Π°. ΠšΠΎΡ€ΠΈΡΡ‚Π΅Ρ›ΠΈ особинС NURBS Π±Π°Π·Π½ΠΈΡ… Ρ„ΡƒΠ½ΠΊΡ†ΠΈΡ˜Π° Ρ€Π°Π·Π²ΠΈΡ˜Π΅Π½Π° јС ΠΌΠ΅Ρ‚ΠΎΠ΄ΠΎΠ»ΠΎΠ³ΠΈΡ˜Π° ΠΏΡ€ΠΎΡ€Π°Ρ‡ΡƒΠ½Π° ΠΈΠ½Ρ‚Π΅Ρ€Π»Π°ΠΌΠΈΠ½Π°Ρ€Π½ΠΈΡ… Π½Π°ΠΏΠΎΠ½Π° Ρƒ засСбном ΠΊΠΎΡ€Π°ΠΊΡƒ, Π½Π°ΠΊΠΎΠ½ ΠΈΠ·Ρ€Π°Ρ‡ΡƒΠ½Π°Π²Π°ΡšΠ° ΠΏΠΎΡ™Π° ΠΏΠΎΠΌΠ΅Ρ€Π°ΡšΠ°. Π˜Π·Ρ€Π°Ρ‡ΡƒΠ½Π°Ρ‚ΠΈ су ΠΈΠ½Ρ‚Π΅Ρ€Π»Π°ΠΌΠΈΠ½Π°Ρ€Π½ΠΈ Π½Π°ΠΏΠΎΠ½ΠΈ ΠΊΠΎΡ€ΠΈΡˆΡ›Π΅ΡšΠ΅ΠΌ Ρ˜Π΅Π΄Π½Π°Ρ‡ΠΈΠ½Π° Ρ€Π°Π²Π½ΠΎΡ‚Π΅ΠΆΠ΅ Π·Π° ΠΏΠ»ΠΎΡ‡Π΅ ΠΌΠΎΠ΄Π΅Π»ΠΎΠ²Π°Π½Π΅ Ρ€Π°Π·Π»ΠΈΡ‡ΠΈΡ‚ΠΈΠΌ Ρ‚Π΅ΠΎΡ€ΠΈΡ˜Π°ΠΌΠ° ΠΏΠΎΠ²Ρ€ΡˆΠΈΠ½ΡΠΊΠΈΡ… носача ΠΈ ΠΏΠΎΠΊΠ°Π·Π°Π½Π° јС ΡšΠΈΡ…ΠΎΠ²Π° Π²Π΅Π»ΠΈΠΊΠ° тачност Ρƒ односу Π½Π° ΠΈΠ½Ρ‚Π΅Ρ€Π»Π°ΠΌΠΈΠ½Π°Ρ€Π½Π΅ Π½Π°ΠΏΠΎΠ½Π΅ добијСнС ΠΈΠ· конститутивних Ρ˜Π΅Π΄Π½Π°Ρ‡ΠΈΠ½Π°. Анализа слободних Π²ΠΈΠ±Ρ€Π°Ρ†ΠΈΡ˜Π° ΠΈ Π±ΠΈΡ„ΡƒΡ€ΠΊΠ°Ρ†ΠΈΠΎΠ½Π΅ стабилности ΠΏΠΎΠΊΠ°Π·Π°Π»Π΅ су високу тачност ΠΌΠ΅Ρ‚ΠΎΠ΄Π°...This doctoral dissertation deals with analysis of laminated composite structures using isogeometric finite element method. In isogeometric analysis same basis functions that are used for geometry representation are also used for approximation of unknown quantities. Isogeometrical mathematical models of laminated thin walled structures are formulated. The proposed models are based on most popular equivalent layer theories, that is Kirchoff-love, Mindlin-Reissner and Reddy's plate theories with the use of NURBS basis functions. Main matrices of finite element method for static, dynamic and stability analysis are formulated for all three plate theories. Relation between displacements and strains are linear, except for the case of stability analysis where standard non-linear procedure is used for geometric stiffness matrix formulation. Constitutive relations are linear. Finite element equations are derived using displacement method, Extensive numerical testing of the proposed method is conducted in order to verify the performance of the method. Obtained results are compared with analytical solutions and other available results. The obtained results demonstrated high accuracy of the method in comparison to the conventional finite element method and existing alternatives. Static analysis of developed models showed high accuracy of the proposed formulation and the advantages of using higher-order basis functions. Using the properties of NURBS basis functions, methodology for interlaminar stress calculation is developed that is able to accurately compute interlaminar stresses in a single separate step, after calculation of displacement field is performed. The interlaminar stresses are calculated using the equilibrium equations for plates modeled with different plate theories. High accuracy of equilibrium interlaminar stresses compared to constitutive interlaminar stresses is demonstrated. Free vibration and buckling analysis also demonstrated high accuracy of the method..

    Assessment results of fluid-structure interaction numerical simulation using fuzzy logic

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    A fuzzy approximation concept is applied in order to predict results of coupled computational structure mechanics and computational fluid dynamics while solving a problem of steady incompressible gas flow through thermally loaded rectangular thin-walled channel. Channel wall deforms into wave - type shapes depending on thermal load and fluid inlet velocity inducing the changes of fluid flow accordingly. A set of fluid - structure interaction (FSI) numerical tests have been defined by varying the values of fluid inlet velocity, temperature of inner and outer surface of the channel wall and numerical grid density. The unsteady Navier-Stokes equations are numerically solved using an element-based finite volume method and second order backward Euler discretization scheme. The structural model is solved by finite element method including geometric and material nonlinearities. The implicit two-way iterative code coupling, partitioned solution approach, were used while solving these numerical tests. Results of numerical analysis indicate that gravity and pressure distribution inside the channel contributes to triggering the shape of deformation. In the inverse problem, the results of FSI numerical simulations formed a database of input variables for development fuzzy logic based models considering downstream pressure drop and maximum stresses as the objective functions. Developed fuzzy models predicted targeting results within a reasonable accuracy limit at lower computation cost compared to series of FSI numerical calculations. Smaller relative difference were obtained when calculating the values of pressure drop then maximal stresses indicating that transfer function influence on output values have to be additionally investigated. [Projekat Ministarstva nauke Republike Srbije, br. III42010, br.TR33050 i br. TR35035

    Isogeometric bending analysis of composite plates based on a higher-order shear deformation theory

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    This research paper presents an isogeometric plate finite element formulation for analysis of thick composite plates. Isogeometric finite element method which is based on non-uniform rational B-splines (NURBS) basis functions, is a novel numerical procedure developed to bridge the gap between CAD and FEM modeling of structures. In order to investigate the behavior of isogeometric plate elements under static loading, plate kinematics is based on third order shear deformation theory (TSDT) of Reddy, which is free from transverse shear locking. This paper discusses accurate transverse stress recovery procedures for TSDT isogeometric finite elements. Numerical experiments with quadratic, cubic and quartic elements are presented and obtained results are compared to other available ones
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