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 63 for “"composite panels"”.

  1. Deformations of Unsymmetric Composite Panels

    … the deformations of various unsymmetric composite panels due to thermal and mechanical loads. Chapter 2 focuses on the warpage of large unsymmetric curved composite panels due manufacturing anomalies. These panels are subjected to a temperature change of -280°F to simulate the cooling …

    vt Repository record for Deformations of Unsymmetric Composite Panels (opens in a new tab)

  2. Simultaneous structural/acoustical design of composite panels

    Since advanced composite materials generally experience coincidence at lower frequencies than metals when used in aircraft fuselage sidewalls, they may allow more transmission of airborne noise thereby requiring heavier acoustical treatments. A sequential design approach of addressing first …

    vt Repository record for Simultaneous structural/acoustical design of composite panels (opens in a new tab)

  3. Thermal and Mechanical Response of Curved Composite Panels

    Curved panels constructed of laminated graphite-epoxy composite material are of potential interest in airframe fuselage applications. An understanding of structural response at elevated temperatures is required for anticipated future high speed aircraft applications. This study concentrates on the …

    vt Repository record for Thermal and Mechanical Response of Curved Composite Panels (opens in a new tab)

  4. Design of Variable Stiffness Composite Panels for Maximum Strength

    … is to explore the design of variable stiffness composites and develop an automated framework to model, analyze and optimize these structures. Variable stiffness composites have been shown to exhibit increased strength and stiffness over traditional constant stiffness composites by tailoring …

    embry-riddle Repository record for Design of Variable Stiffness Composite Panels for Maximum Strength (opens in a new tab)

  5. Structural response and damage development of cylindrical composite panels

    Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.

    mit Repository record for Structural response and damage development of cylindrical composite panels (opens in a new tab)

  6. Investigation of curved composite panels under high-g loading

    … work was conducted to investigate the use of composites within the Wide Area Surveillance Projectile (WASP) wing system by specifically studying the buckling behavior of curved composite panels under high-g loading. A finite element model was developed as a design tool to model the original …

    mit Repository record for Investigation of curved composite panels under high-g loading (opens in a new tab)

  7. Compression and buckling of composite panels with curvilinear fibers

    … response for a symmetrically laminated composite panel with a spatially varying fiber orientation has been analyzed for four different boundary conditions. Variation of the fiber angle along the length of a composite laminate results in stiffness properties that change as a function of …

    vt Repository record for Compression and buckling of composite panels with curvilinear fibers (opens in a new tab)

  8. Thermal Analysis and Response of Grid-Stiffened Composite Panels

    … buckling loads of rectangular grid-stiffened composite panels is presented. Two edge conditions are considered for the panel, one in which all panel edges are free to deform, and another when all the edges are restrained. In the first case panel deformations due to a uniformly distributed …

    vt Repository record for Thermal Analysis and Response of Grid-Stiffened Composite Panels (opens in a new tab)

  9. Combined structural and manufacturing optimization of stiffened composite panels

    … the design optimization of a blade-stiffened composite panel. For the manufacturing analysis, a one-dimensional resin film infusion model is developed to compute the infiltration time of the resin into a fabric preform of the panel. Results are presented showing the effects of structurally …

    vt Repository record for Combined structural and manufacturing optimization of stiffened composite panels (opens in a new tab)

  10. Large deformation behavior of long shallow cylindrical composite panels

    … experimental apparatus was designed to load the panels. Experimental results of displacement controlled tests performed on graphite-epoxy curved panels are compared with analytic predictions. This study demonstrates that panel shallowness, material orthotropy, and stacking sequence can influence …

    vt Repository record for Large deformation behavior of long shallow cylindrical composite panels (opens in a new tab)

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

    … 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 of simply …

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

  12. Structural acoustic analysis of shape memory alloy hybrid composite panels

    Shape memory alloy (SMA) hybrid adaptive composites are a class of materials which combine the strain recovery and elastic properties transformation capabilities of SMA fibers with the structural characteristics of advanced composite materials. This study utilizes the Rayleigh-Ritz method and …

    vt Repository record for Structural acoustic analysis of shape memory alloy hybrid composite panels (opens in a new tab)

  13. Calculation of skin-stiffener interface stresses in stiffened composite panels

    … skin-stiffener interface stresses in stiffened composite panels is developed. Both geometrically linear and nonlinear analyses are considered. Particular attention is given to the flange termination region where stresses are expected to exhibit unbounded characteristics. The method is based on a …

    vt Repository record for Calculation of skin-stiffener interface stresses in stiffened composite panels (opens in a new tab)

  14. Optimal stacking sequence design of stiffened composite panels with cutouts

    The growing use of high performance composite materials has stimulated interest in the development of optimization procedures for the design of laminates. The design of composite structures against buckling presents two major challenges to the structural analyst and designer. First, the problem of …

    vt Repository record for Optimal stacking sequence design of stiffened composite panels with cutouts (opens in a new tab)

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

    … 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 solution. The …

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

  16. Advanced thermal insulation for energy efficient buildings : structural performance of aerogel composite panels

    … low mechanical properties. We then propose a composite structure for a rigid aerogel panel, a sandwich panel with a truss core filled with monolithic aerogel. Mechanical and thermal properties are derived and partially tested for the truss cores. Several designs are studied and mechanical …

    mit Repository record for Advanced thermal insulation for energy efficient buildings : structural performance of aerogel composite panels (opens in a new tab)

  17. Prebuckling and postbuckling behavior of stiffened composite panels with axial-shear stiffness coupling

    To advance structural tailoring methods in composite structures, an experimental and numerical investigation of the prebuckling and postbuckling responses of flat rectangular graphite-epoxy composite panels with a centrally located I-shaped stiffener subjected to a uniform end shortening is …

    vt Repository record for Prebuckling and postbuckling behavior of stiffened composite panels with axial-shear stiffness coupling (opens in a new tab)

  18. A new scheme for the optimum design of stiffened composite panels with geometric imperfections

    Thin walled stiffened composite panels, which are among the most utilized structural elements in engineering, possess the unfortunate property of being highly sensitive to geometrical imperfections. Existing analysis codes are able to predict the nonlinear postbuckling behavior of a structure with …

    vt Repository record for A new scheme for the optimum design of stiffened composite panels with geometric imperfections (opens in a new tab)

  19. The response of concave singly curved fibre reinforced moulded sandwich and laminated composite panels to blast loading

    Composite materials are increasingly being used in a wide range of structural applications. These applications range from bicycle frames and building facades to hulls of marine ships. Their popularity is due to the high specific strength and stiffness properties, corrosion resistance, and the …

    cape-town Repository record for The response of concave singly curved fibre reinforced moulded sandwich and laminated composite panels to blast loading (opens in a new tab)

Page 1 of 4