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
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;
Conference_Titel :
Aerospace Conference, 2004. Proceedings. 2004 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
0-7803-8155-6
DOI :
10.1109/AERO.2004.1368071