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Droplets evolution

To provide sufficient time for the droplet evolution, one can increase the distance between the ES capillary and the sampling orifice or sampling capillary. However, this reduces greatly the sampling efficiency since the charged droplet density and... [Pg.270]

Because the computational cost of performing a 3-D transient simulation is quite high, an axisymmetric 2-D approximation of the tube bank was also considered. A column of spheres of the same diameter and spacing as the tubes was modeled using a mesh similar to the 3-D case. It was found that several 2-D models with varying initial film thickness inputs all significantly under-predicted the droplet size and the time for droplet evolution. [Pg.362]

Fig. 32.18 Droplet evolution due to solvent evaporation and droplet jet fission (Reprinted with... Fig. 32.18 Droplet evolution due to solvent evaporation and droplet jet fission (Reprinted with...
Figure 30.17 Water droplet evolution in a microchannel with smooth hydrophilic surface predicted by VOF (a) [61] and (b) [62]. Figure 30.17 Water droplet evolution in a microchannel with smooth hydrophilic surface predicted by VOF (a) [61] and (b) [62].
When the sprayed solution contains a solute, such as a salt, the continuous evaporation of the droplets will lead to very high concentrations of the salt and finally to charged solid partides - skeletons of the charged droplets that can reveal some aspects of the droplet evolution. Fernandez de la Mora and coworkers [32] have used this approach to study charged droplet evolution. This work is of special relevance to the ion evaporation model and is discussed in Section 1.2.8. [Pg.11]

A droplet evolution scheme is shown in Figure 1.5. It deals with droplets produced by nanoelectrospray. Nanospray (see Section 1.2.4) is a technique that considerably... [Pg.13]

From the standpoint of the mechanism of ESI, an agreement of the Kas values determined via ESI-MS with values obtained with conventional in-solution methods may appear surprising. One could expect that the very large increase in the concentration of the solutes in the charged droplets due to evaporation of the solvent in the droplet evolution will lead to an apparent Kas that is much too high. However, this equilibrium shift need not occur if rates of the forward and reverse reactions leading to the equilibrium are slow compared to the time of droplet evaporation. [Pg.30]

Fig. 1.32 a Mechanical decomposition of a droplet from an electrospray source. Taken from [99]. b Scheme of droplet evolution during the electrospray process as a result of solvent evaporation and fission. Adapted from [103]... [Pg.33]

The assumptions with which the scheme (Figure 1.6) for water as solvent was obtained are described in detail in the section entitled Calculations and Experimental in Peschke et al. The stability limits of droplet fission at droplet charge Z=0.9Z/ (just before the droplet fission) and Z = 0.1 Zr (just after the fission due to Beauchamp and co-workers for water) were used (see Figure 1.4 in the present work). These are for droplets of radii in the 13- to 3-pm range, while the nano-droplet evolution scheme (Figure 1.6) involves close to a hundred times smaller radii. It is not known to what extent the droplet fissions of such small droplets follow the same stability limits. Unfortunately, no measurements for such small droplets exist because these droplets evaporate and fission very fast, within several microseconds, while the large droplets fission within intervals of some 40 ms (see Figure 1.4). [Pg.18]

Droplet Dispersion. The primary feature of the dispersed flow regime is that the spray contains generally spherical droplets. In most practical sprays, the volume fraction of the Hquid droplets in the dispersed region is relatively small compared with the continuous gas phase. Depending on the gas-phase conditions, Hquid droplets can encounter acceleration, deceleration, coUision, coalescence, evaporation, and secondary breakup during thein evolution. Through droplet and gas-phase interaction, turbulence plays a significant role in the redistribution of droplets and spray characteristics. [Pg.330]

Then the mixture with droplets is quenched into the spinodal instability region to some T < Ta (Concentration c(r) within droplets starts to evolve towards the value C(,(T) > C(,(T ), but the evolution type depends crucially on the value Act = cj(T) — Ch(Ta). At small Act we have a usual diffusion with smooth changes of composition in space and time. But when Act is not mall (for our simulations Act O.2), evolution is realised via peculiar wave-like patterning shown in Figs. 8-10. [Pg.108]

D. Evolution of Initial Charged Droplets to Very Small... [Pg.255]

Unfortunately, the conflict has not been resolved.36 However from the standpoint of the experimentalist, many of the consequences of the two theories are similar. Both theories require very small droplets to generate gas-phase ions. The time requirement for the evolution to such droplets (see Figure 2) is in the hundreds of microseconds. The ambient gas is essential to provide the thermal energy for the evaporation. Solvents with low vapor pressure and condensation coefficients a may not be suitable or may require higher ambient temperatures. [Pg.270]

Figure 20. An example of the pattern evolution during the viscoelastic phase separation [165] There is a frozen period after the quench nucleation of the less viscous phase in a droplet pattern the volume shrinking of the more viscous phase transient formation of the bicontinuous network structure phase inversion in the final stage. This figure has been kindly provided by Dr. T. Araki. Figure 20. An example of the pattern evolution during the viscoelastic phase separation [165] There is a frozen period after the quench nucleation of the less viscous phase in a droplet pattern the volume shrinking of the more viscous phase transient formation of the bicontinuous network structure phase inversion in the final stage. This figure has been kindly provided by Dr. T. Araki.
Fig. 14 shows the comparison of the photographs from Chandra and Avedisian (1991) with simulated images of this study for a subcooled 1.5 mm n-heptane droplet impact onto a stainless-steel surface of 200 °C. The impact velocity is 93 cm/s, which gives a Weber number of 43 and a Reynolds number of 2300. The initial temperature of the droplet is room temperature (20 °C). In Fig. 14, it can be seen that the evolution of droplet shapes are well simulated by the computation. In the first 2.5 ms of the impact (frames 1-2), the droplet spreads out right after the impact, and a disk-like shape liquid film is formed on the surface. After the droplet reaches the maximum diameter at about 2.1ms, the liquid film starts to retreat back to its center (frame 2 and 3) due to the surface-tension force induced from the periphery of the droplet. Beyond 6.0 ms, the droplet continues to recoil and forms an upward flow in the center of the... [Pg.43]


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See also in sourсe #XX -- [ Pg.11 , Pg.13 ]




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