07.02.2013 Views

Scientific and Technical Aerospace Reports Volume 39 April 6, 2001

Scientific and Technical Aerospace Reports Volume 39 April 6, 2001

Scientific and Technical Aerospace Reports Volume 39 April 6, 2001

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

current is caused by the impurity content (O2, 0.107%) in CO2 gas source. In region II, the cell’s current stays at a nearly constant<br />

level although the CO2 electrode potential increases in magnitude. The anodic activation overpotential at the oxygen side remains<br />

unchanged, while the cathodic overpotential increased sharply. At this point, all O2 taking part in electrochemical reaction comes<br />

from O2 impurity of CO2. There is no CO2 dissociating into CO <strong>and</strong> O. Because of limited O2 source, the cell is in a mass limited<br />

flow condition. All the increase in applied potential is utilized at the cathode, while the activation overpotential on anode side<br />

remains unchanged. The overpotential at the cathode side is still not sufficient to provide the free energy required to crack CO2.<br />

In region III, the cell’s current increases with applied voltage, after the CO2 electrode voltage reaches a certain threshold value.<br />

The activation overpotential at CO2 side drops sharply, while activation overpotential on the anode side increases. The magnitude<br />

of the threshold is a function of temperature. It can be determined by the CO2 energy of formation <strong>and</strong> is termed the Nernst potential.<br />

In region III the activation overpotentials fit the Tafel plot well. The data on exchange current density <strong>and</strong> charge transfer<br />

coefficients obtained from the Tafel plots can be used to fit the well known Butler Volmer equation. SOECs have been used in<br />

a CO2 environment to produce O2. The current-voltage characteristics <strong>and</strong> overpotentials associated with the process have been<br />

measured. Three distinct regions are observed, <strong>and</strong> been analyzed.<br />

Author (revised)<br />

Solid Oxide Fuel Cells; Ceramics; Electric Potential; Electrolytic Cells; Electrolytes; Ionic Mobility; Ion Motion<br />

<strong>2001</strong>0024909 Johns Hopkins Univ., Dept. of Mechanical Engineering, Baltimore, MD USA<br />

Production <strong>and</strong> Removal of Gas Bubbles in Microgravity<br />

Oguz, H. N., Johns Hopkins Univ., USA; Proceedings of the Fifth Microgravity Fluid Physics <strong>and</strong> Transport Phenomena Conference;<br />

December 2000, pp. 462-463; In English; See also <strong>2001</strong>0024890; No Copyright; Abstract Only; Available from CASI only<br />

as part of the entire parent document<br />

This study focuses on two topics relevant in many microgravity applications: formation of gas bubbles from orifices in tubes<br />

<strong>and</strong> removal of individual bubbles from liquids. Bubble injection from an axisymmetric slot is investigated experimentally <strong>and</strong><br />

numerically. Three dimensional boundary integral simulations of bubble injection from multiple holes along the axial direction<br />

of a tube have also been carried out. Several difficulties encountered in the numerical modeling of these flows have been overcome<br />

<strong>and</strong> a stable method has been developed. The main difficulty is the tendency of a growing bubble to touch nearby solid surfaces.<br />

An artificial force is introduced to keep bubbles away from the walls <strong>and</strong> continue the computations without affecting the main<br />

characteristics of the problem. It has been observed that downstream bubbles detach earlier when all bubbles start growing at the<br />

same time. This is expected because the average flow rate seen by downstream bubbles is higher than the ones seen by upstream<br />

bubbles. Bubble shapes obtained from normal gravity experiments are shown in fig. 1. Simulations under similar flow condition<br />

reproduce this flow. A series of experiments have been carried out to investigate gas injection from an axisymmetric slot in a tube<br />

under normal gravity conditions. Three distinct regimes of operation as a function of the gas/liquid flow rate ratios are observed.<br />

At high gas flow rates, the injected gas completely fills the tube <strong>and</strong> blocks the liquid flow. A Taylor bubble is generated in this<br />

regime. When the liquid flow rate becomes comparable to the gas injection rate, axial symmetry is broken <strong>and</strong> a regular single<br />

bubble forms. This is identified as the second regime where the liquid flow is not interrupted by the gas. At even higher liquid<br />

flow rates, turbulent conditions <strong>and</strong> chaotic multi-bubble formations are observed. This is the third regime. Illustrative pictures<br />

for these regimes are shown. An axisymmetric boundary integral code is employed to simulate this flow. Because of the imposed<br />

symmetry the range of validity of the simulations were somewhat limited but the results are useful in underst<strong>and</strong>ing the basic<br />

dynamics of the problem. Simulations suggest the existence of a stable liquid column inside the bubble. Assuming that the bubble<br />

front moves with the same velocity as the liquid column, an equilibrium condition that admits one stable solution is derived.<br />

Although there have been many investigations of the formation of bubbles from an underwater orifice, the opposite case, i.e.<br />

removal of bubbles by an orifice, has received very little attention. The dynamics of a bubble entering a capillary tube is studied.<br />

A stream of sparsely spaced bubbles generated from an underwater orifice is positioned just below a capillary tube that is connected<br />

to a vacuum reservoir. Sufficiently small bubbles are captured in the capillary. In some cases, a small bubble detaches from<br />

the back of the main one as a result of severe surface deformation near the entrance of the capillary. Larger bubbles, on the other<br />

h<strong>and</strong>, break in two while being drawn into the capillary. A boundary integral technique is employed to simulate this process. An<br />

artificial repulsive force is introduced to form a thin layer of water around the bubble in the capillary tube. With this scheme, it<br />

is possible to simulate bubble motion both outside <strong>and</strong> inside the capillary. Numerical bubble shapes are found to be in very good<br />

agreement with experiment.<br />

Author (revised)<br />

Bubbles; Gas Flow; Gas Injection; Microgravity; Slots; Gas-Liquid Interactions<br />

76

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!