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They also concluded that the nature of middle-phase microemulsion was very complicated and that its microstructure involves an intermicellar equilibrium incorporating various types of droplets, bicontinuous fluctuating and/or a rigid liquid crystal phase states, depending on the type of salt in the system.
The coalescence of nearly rigid liquid droplets in a turbulent flow field is viewed as the drainage of a thin film of liquid under the action of a stochastic force representing the effect of turbulence.
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However, in the case of a nearly microporous adsorbent, the diffusivity appears to be dependent on temperature to an extent which is not consistent with the assumption of diffusion in rigid, liquid-filled pores.
Lopez et al. (2010) hypothesized that this could correspond to the lateral segregation of MSM and cholesterol in rigid liquid-ordered (Lo) phase microdomains surrounded by the fluid matrix of glycerophospholipids in the liquid-disordered (Ld) phase.
As a locus for the integration of key cellular functions and signalling (Hayashi et al, 2009), MAM apparently requires a more rigid liquid-ordered phase to recruit, orient, regulate, and limit the lateral mobility of the membrane proteins within its boundaries, so as to promote the cross-talk of mitochondria and ER.
In [17], the comprehensive optimization of rigid tool Liquid composite molding (LCM) processes was established as a BLOP.
Depending on temperature, the polymer phases can vary from solid (rigid) to liquid (mobile).
A comprehensive tooling force analysis is presented for rigid tool Liquid Composite Moulding (LCM) processes such as Resin Transfer Moulding (RTM) and Injection/Compression Moulding (I/CM).
The presented nonlinear system model can provide an important reference for the overall design of the modern spacecraft composed of rigid platform, liquid filled tank and flexible appendage.
The seismic response of partially-filled two-dimensional rigid rectangular liquid tanks with a bottom-mounted submerged block is numerically simulated.
The Lagrangians of the main body of the spacecraft (rigid tank), liquid, and two beams (flexible appendages) were used in addition to assuming symmetric motion of the system; the frequency equations of the coupled system were obtained by applying the Rayleigh Ritz method.
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