A semi-analytical model for local post-buckling analysis of stringer- and frame-stiffened cylindrical panels
A fast semi-analytical model for the post-buckling analysis of stiffened cylindrical panels is presented. The panel is comprised of a skin (shell) and stiffeners in both longitudinal (stringers) and circumferential direction (frames). Local buckling modes are considered where the skin may buckle wit...
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| Vydáno v: | Thin-walled structures Ročník 44; číslo 1; s. 102 - 114 |
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| Hlavní autoři: | , , , |
| Médium: | Journal Article |
| Jazyk: | angličtina |
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Oxford
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2006
New York, NY Elsevier Science |
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| ISSN: | 0263-8231, 1879-3223 |
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| Abstract | A fast semi-analytical model for the post-buckling analysis of stiffened cylindrical panels is presented. The panel is comprised of a skin (shell) and stiffeners in both longitudinal (stringers) and circumferential direction (frames). Local buckling modes are considered where the skin may buckle within a bay and may induce rotation of the stiffeners. Stringers and frames are considered as structural elements and are thus not ‘smeared’ onto the skin. Large out-of-plane deflections and thus non-linear strain–displacement relations of skin and stiffeners are taken into account. The displacements of skin and stiffeners are approximated by trigonometric functions (Fourier series). First, a linear buckling eigenvalue analysis is carried out and some combination of buckling eigenmodes is chosen as imperfection. Then the load history is started and the Fourier coefficients are determined by minimizing the stiffened panel's energy at each load level. A curve-tracing algorithm, the Riks method, is used to solve the equations. The present model can be used to assess the post-buckling behavior of stiffened panels, for example, aircraft fuselage sections. |
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| AbstractList | A fast semi-analytical model for the post-buckling analysis of stiffened cylindrical panels is presented. The panel is comprised of a skin (shell) and stiffeners in both longitudinal (stringers) and circumferential direction (frames). Local buckling modes are considered where the skin may buckle within a bay and may induce rotation of the stiffeners. Stringers and frames are considered as structural elements and are thus not 'smeared' onto the skin. Large out-of-plane deflections and thus non-linear strain-displacement relations of skin and stiffeners are taken into account. The displacements of skin and stiffeners are approximated by trigonometric functions (Fourier series). First, a linear buckling eigenvalue analysis is carried out and some combination of buckling eigenmodes is chosen as imperfection. Then the load history is started and the Fourier coefficients are determined by minimizing the stiffened panel's energy at each load level. A curve-tracing algorithm, the Riks method, is used to solve the equations. The present model can be used to assess the post-buckling behavior of stiffened panels, for example, aircraft fuselage sections. |
| Author | Tessmer, Jan Schagerl, Martin Buermann, Philipp Rolfes, Raimund |
| Author_xml | – sequence: 1 givenname: Philipp surname: Buermann fullname: Buermann, Philipp email: philipp.buermann@dlr.de organization: DLR, Institute of Structural Mechanics, Structural Analysis Section, Lilienthalplatz 7, 38108 Braunschweig, Germany – sequence: 2 givenname: Raimund surname: Rolfes fullname: Rolfes, Raimund organization: Airbus Deutschland GmbH, ESAS, Kreetslag 10, 21129 Hamburg, Germany – sequence: 3 givenname: Jan surname: Tessmer fullname: Tessmer, Jan organization: Airbus Deutschland GmbH, ESAS, Kreetslag 10, 21129 Hamburg, Germany – sequence: 4 givenname: Martin surname: Schagerl fullname: Schagerl, Martin organization: Airbus Deutschland GmbH, ESAS, Kreetslag 10, 21129 Hamburg, Germany |
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| Keywords | Post-buckling Large deflection theory Local buckling model Panel buckling Semi-analytical Stiffened cylindrical shell High strain Localized mode Displacement(deformation) Modeling Energy level Trigonometric series Structural frame Local buckling Defect Eigenvalue problem Buckling Civil engineering Stiffener Eigenmode Frame construction Mechanical properties Fourier series Postbuckling Reinforced structure Reinforced shell Trigonometric function Cylindrical shell Non linear effect Aircraft |
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| SubjectTerms | Buckling Exact sciences and technology Fundamental areas of phenomenology (including applications) Large deflection theory Local buckling model Panel buckling Physics Post-buckling Semi-analytical Solid mechanics Stiffened cylindrical shell Structural and continuum mechanics |
| Title | A semi-analytical model for local post-buckling analysis of stringer- and frame-stiffened cylindrical panels |
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