• DocumentCode
    2109878
  • Title

    Elastic parameters of nanoclay-reinforced polymers for space and launch vehicles

  • Author

    Mallick, Kaushik ; Paul, Lt Chris

  • Author_Institution
    Composite Technol. Dev. Inc., Lafayette, CO, USA
  • Volume
    4
  • fYear
    2004
  • fDate
    13-13 March 2004
  • Firstpage
    2740
  • Abstract
    The present study derives an analytical expression for the effective elastic modulus of nanoclay-reinforced polymer matrix. The motivation behind the current work is that the usual rule of mixture calculations provides very poor estimates of the elastic parameters of the composite. A micromechanics based model and effective elastic continuum theory are used to derive the effective moduli of an elastic medium embedded with rectilinear inclusions representing disk like nanoclay particles. For simplicity a spatially distributed parallel array of nanoclay dispersion is considered in the current analysis. The effective modulus of the composite is derived in terms of the volume fraction of the nanoclays and the elastic parameters of the virgin matrix and the nanoclay particles.
  • Keywords
    clay; continuum mechanics; elastic moduli; fibre reinforced plastics; filled polymers; inclusions; micromechanics; nanocomposites; nanoparticles; space vehicles; composite materials; effective elastic continuum theory; effective elastic moduli; elastic parameters; launch vehicles; micromechanics based model; nanoclay dispersion; nanoclay particles; nanoclay-reinforced polymer matrix; rectilinear inclusions; space vehicles; spatially distributed parallel array; volume fraction; Amorphous materials; Composite materials; Laboratories; Nanocomposites; Nanoparticles; Nanotechnology; Polymers; Sheet materials; Space technology; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2004. Proceedings. 2004 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    0-7803-8155-6
  • Type

    conf

  • DOI
    10.1109/AERO.2004.1368071
  • Filename
    1368071