1–8 von 8 Ergebnissen
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    Buckling of Composite Plates

    Kassapoglou, Christos | Wiley | 2010
    Schlagwörter: approximate and exact buckling loads ‐ function of panel aspect ratio , rectangular composite plate buckling ‐ under biaxial loading , composite plates under compression ‐ and/or shear loading, sensitive to buckling failures , composite plate buckling , buckling of rectangular composite plate under shear ‐ rectangular composite plate under shear , composite plate under compression and shear , post‐buckling of composite plates ‐ accurate knowledge of possible failure modes and potential interactions , buckling of rectangular composite plate ‐ and uniaxial compression

    Composite Structural Components and Mathematical Formulation

    Kassapoglou, Christos | Wiley | 2010
    Schlagwörter: governing equations for a composite plate ‐ and energy methods, as powerful alternatives , simplified flow diagram ‐ of design/structural analysis process , composite structural components and mathematical formulation ‐ composite airframe , part families, in a composite airframe , types of parts making up airframe, fuselage and/or wing ‐ being same for metal and composite structures

    Applications of Advanced Composites in Aircraft Structures

    Kassapoglou, Christos | Wiley | 2010
    Schlagwörter: Beech Starship I, on heels of Lear Fan ‐ first all‐composite airplane to obtain FAA certification , composite application in civilian or military aircrafts ‐ typical stages, new technology intoduced during its implementation , application of composites on primary aircraft structure ‐ Boeing 777, in 1990s , implementation of composites in aircraft structure ‐ examining amount of composites (by weight) in aircraft models as function of time , first application of advanced composites ‐ on Akaflieg Phönix FS‐24 , advanced composite applications ‐ in aircraft structures

    Post‐Buckling

    Kassapoglou, Christos | Wiley | 2010
    Schlagwörter: ability of plates to withstand load in post‐buckling regime ‐ without failing, making configurations attractive for design , post‐buckled stiffened composite plate under shear , postbuckling angle, as function of applied shear load , post‐buckled curved composite stiffened panel , significant load carrying ability beyond buckling ‐ ability, capitalized in generating designs of lighter weight , post‐bucking analysis ‐ of composite panels under compression

    Review of Classical Laminated Plate Theory

    Kassapoglou, Christos | Wiley | 2010
    Schlagwörter: basic laminate definitions and summary of classical laminated‐plate theory (CLPT) , ‘composite material’ ‐ fiber and matrix mixture, and configurations combining some of the best characteristics of two constituents , orthotropic materials, possessing two planes of symmetry

    Design and Analysis of Composite Beams

    Kassapoglou, Christos | Wiley | 2010
    Schlagwörter: composite beams ‐ design and analysis , additional guidelines, built on the basis of experience ‐ and good engineering practice , fastener spacing and flange stiffness ‐ determining failure modes of flange , axial (EA) and bending (EI) stiffnesses of beam ‐ accurate determination of values for a composite cross‐section, important

    Good Design Practices and Design ‘Rules of Thumb’

    Kassapoglou, Christos | Wiley | 2010
    Schlagwörter: good design practices and design ‘Rules of Thumb’ , bending stiffness improvement ‐ of one‐dimensional composite structure , stiffener cross‐section ‐ created on basis of design guidelines , design guidelines, result of analysis and trending, test results and experience , methods in assembling ‐ bolted connections, bonded connections, co‐cured with use of 3‐D preform , fastener rules of thumb and Plydrop guidelines

    Sandwich Structure

    Kassapoglou, Christos | Wiley | 2010
    Schlagwörter: composite laminates and facesheets ‐ materials and configurations of foam, honeycomb, low density foaming aluminum , buckling load of sandwich with and without transverse shear effects ‐ function of core thickness , wrinkling, local buckling phenomenon ‐ facesheet of sandwich buckling over characteristic half‐wavelength , attaching sandwich structures ‐ difficulty in attaching to adjacent structures, limiting usage of sandwich structure , sandwich structure, of two facesheets ‐ separated by lightweight core , bending of sandwich panel ‐ under compression