Global ETD Search

Search theses and dissertations gathered from participating repositories worldwide. Every result links back to the library that holds it. No account is needed.

Results

Showing 1 to 20 of 32 for “"stiffened panels"”.

  1. Consequences of Simultaneous Local and Overall Buckling in Stiffened Panels

    … panel buckling of uniaxially compressed T-stiffened panels are developed and validated with 55 ABAQUS eigenvalue buckling analyses of a wide range of typical panel geometries. These two expressions are equated to derive a new expression for the rigidity ratio (EIx/Db)CO that uniquely …

    vt Repository record for Consequences of Simultaneous Local and Overall Buckling in Stiffened Panels (opens in a new tab)

  2. High Performance Algorithms for Structural Analysis of Grid Stiffened Panels

    … engineering problem, structural analysis of grid stiffened panels. An existing engineering code, SPANDO, is studied and modified to execute more efficiently on high performance workstations and parallel computers. Two new SPANDO packages, a modified sequential SPANDO and parallel SPANDO, are …

    vt Repository record for High Performance Algorithms for Structural Analysis of Grid Stiffened Panels (opens in a new tab)

  3. Buckling Analysis of Composite Stiffened Panels and Shells in Aerospace Structure

    Stiffeners attached to composite panels and shells may significantly increase the overall buckling load of the resultant stiffened structure. Initially, an extensive literature review was conducted over the past ten years of published work wherein research was conducted on grid stiffened composite …

    vt Repository record for Buckling Analysis of Composite Stiffened Panels and Shells in Aerospace Structure (opens in a new tab)

  4. Minimum-weight design of compressively loaded stiffened panels for postbuckling response

    … preliminary design of minimum-weight thin-walled stiffened composite panels loaded in uniaxial compression based on a geometrically nonlinear analysis. An approximate, semi-analytical nonlinear analysis code, NLPAN, which requires buckling eigenfunction information from the buckling analysis code, …

    vt Repository record for Minimum-weight design of compressively loaded stiffened panels for postbuckling response (opens in a new tab)

  5. Ultimate Strength Analysis of Stiffened Panels Using a Beam-Column Method

    … for studying the ultimate strength problems of stiffened panels with two load cases: 1) under longitudinal compression, and 2) under transverse compression. Chapter 2 presents an improved step-by-step numerical integration procedure based on (Chen and Liu, 1987) to calculate the ultimate …

    vt Repository record for Ultimate Strength Analysis of Stiffened Panels Using a Beam-Column Method (opens in a new tab)

  6. Global-local Finite Element Fracture Analysis of Curvilinearly Stiffened Panels and Adhesive Joints

    … to study the damage tolerance of curvilinearly stiffened panels; fabricated using the modern additive manufacturing process, the so-called unitized structures, and that of adhesive joints. A damage tolerance study of the unitized structures requires cracks to be defined in the vicinity of the …

    vt Repository record for Global-local Finite Element Fracture Analysis of Curvilinearly Stiffened Panels and Adhesive Joints (opens in a new tab)

  7. Uncertainty in marine structural strength with application to compressive failure of longitudinally stiffened panels

    … to the compressive failure of longitudinally stiffened panels. The strength prediction model used in this analysis was developed in the UK and is widely used in analysis and design. Several experimental sample sets are used in the analysis. Mean values and coefficients of variation are …

    vt Repository record for Uncertainty in marine structural strength with application to compressive failure of longitudinally stiffened panels (opens in a new tab)

  8. Validation of the ULSAP Closed-Form Method for Ultimate Strength Analysis of Cross-Stiffened Panels

    … Riks ultimate strength analyses of cross-stiffened panels. These panels cover a wide range of typical geometries. Uniaxial compression is applied to the panels, and in some cases combined with lateral pressure. For eight of the panels full-scale experimental results are available, and …

    vt Repository record for Validation of the ULSAP Closed-Form Method for Ultimate Strength Analysis of Cross-Stiffened Panels (opens in a new tab)

  9. Combined Compression and Shear Structural Evaluation of Stiffened Panels Fabricated Using Electron Beam Freeform Fabrication

    … structures. The structural efficiency of blade stiffened panels made with EBF3 was compared to panels made by integrally machining from thick plate. The panels were tested under two load cases in a combined compression-shear load test fixture. One load case tested the panels' responses to a …

    vt Repository record for Combined Compression and Shear Structural Evaluation of Stiffened Panels Fabricated Using Electron Beam Freeform Fabrication (opens in a new tab)

  10. Structural analysis of geodesically stiffened composite panels with variable stiffener distribution

    … to predict buckling load of geodesically stiffened composite panels under in-plane loads. The analysis procedure accounts for the contribution of the in-plane extensional and out-of-plane bending stiffnesses of the stiffeners through the use of Lagrange multipliers in an energy method …

    vt Repository record for Structural analysis of geodesically stiffened composite panels with variable stiffener distribution (opens in a new tab)

  11. Flutter of rectangular simply supported panels at high supersonic speeds

    … however, to other panel configurations. Clamped panels, integrally stiffened panels, arrays of panels, end others should be amenable to treatment by the model approach based on the static aerodynamic approximation.

    vt Repository record for Flutter of rectangular simply supported panels at high supersonic speeds (opens in a new tab)

  12. Piezoelectric Control of Structures Prone to Instabilities

    Thin-walled structures such as stiffened panels fabricated out of high strength materials are ubiquitous in aerospace structures. These are prone to buckle in a variety of modes with strong possibility of adverse interaction under axial compression and/or bending. Optimally designed stiffened

    wustl Repository record for Piezoelectric Control of Structures Prone to Instabilities (opens in a new tab)

  13. Structural analysis and optimum design of geodesically stiffened composite panels

    … to predict the buckling of geodesically stiffened composite panels under in-plane loads. This procedure accounts for the discrete flexural contribution of each stiffener through the use of Lagrange multipliers in an energy method solution. An analysis is also implemented for the buckling …

    vt Repository record for Structural analysis and optimum design of geodesically stiffened composite panels (opens in a new tab)

  14. Vibro-acoustic optimization of panel with curvilinear stiffeners

    … easy to manufacture complex shapes such as panels with curvilinear stiffeners. Designing and optimizing stiffened panels with predefined structural and acoustic response is the focus of this dissertation. Researchers have dealt with sizing optimization of panels with straight/curvilinear …

    vt Repository record for Vibro-acoustic optimization of panel with curvilinear stiffeners (opens in a new tab)

  15. A method for the geometrically nonlinear analysis of compressively loaded prismatic composite structures

    … analysis of the static response of thin-walled stiffened composite structures loaded in uniaxial or biaxial compression. The method is applicable to arbitrary prismatic configurations composed of linked plate strips, such as stiffened panels and thin-walled columns. The longitudinal ends of the …

    vt Repository record for A method for the geometrically nonlinear analysis of compressively loaded prismatic composite structures (opens in a new tab)

  16. Fracture of aluminum naval structures

    … and mechanics of fracture that govern naval stiffened panels. Therefore, a comprehensive tool consisting of application of advanced fracture models, material calibration, and validation through component testing is provided that will increase the survivability envelope and speed up the …

    mit Repository record for Fracture of aluminum naval structures (opens in a new tab)

  17. Inelastic Analysis of Tripping Failure of Stiffened Steel Panels due to Stiffener Flange Transverse Initial Eccentricity

    … to predict the ultimate tripping strength of stiffened panels under compressive axial stress. The current methods involve the use of a bifurcation, or eigenvalue, approach to predicting failure stress. The effects of initial transverse eccentricity of the stiffener are ignored using such a …

    vt Repository record for Inelastic Analysis of Tripping Failure of Stiffened Steel Panels due to Stiffener Flange Transverse Initial Eccentricity (opens in a new tab)

  18. Bonded structures for enhanced damage tolerant pressurized fuselages

    … to the specific structural concept. Large flat stiffened panels that combine MLs and selective reinforcements have been tested with the purpose of investigating solutions applicable to pressurized fuselages. The large test campaign (for a total of 35 stiffened panels) has quantitatively …

    bologna Repository record for Bonded structures for enhanced damage tolerant pressurized fuselages (opens in a new tab)

  19. Resistência última de navios e plataformas danificados por colisões

    … with reduced intact and damaged models of stiffened panels and box girders. Results are expected to increase understanding of structural failure mechanisms, considering damages ranging from small dents to extensive damage to a large area of a ship's hull or FPSO-type platform.

    brazil-uerj Repository record for Resistência última de navios e plataformas danificados por colisões (opens in a new tab)

Page 1 of 2