29.03.2013 Views

Rowan-Gollan-PhD-Thesis - Mechanical Engineering - University of ...

Rowan-Gollan-PhD-Thesis - Mechanical Engineering - University of ...

Rowan-Gollan-PhD-Thesis - Mechanical Engineering - University of ...

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.

50 Chemical Nonequilibrium Chapter 4<br />

takes for the gas particle to pass through the bow shock and transit the vehicle shock layer.<br />

After passing the shock, the thermally perfect gas particle has an excess <strong>of</strong> sensible internal<br />

energy 1 and during subsequent collisions the gas particle will seek to redistribute that energy<br />

among other modes, including chemical energy if available. In particular, molecules will seek<br />

to break chemical bonds as a means <strong>of</strong> absorbing the excess internal energy. For certain flow<br />

conditions, <strong>of</strong>ten associated with flows tending towards the rarefied limit, the amount <strong>of</strong> time<br />

required for sufficient collisions for equilibrium is <strong>of</strong> the same order as the time required for a<br />

gas particle to transit the shock layer. In these cases, the modelling <strong>of</strong> chemical nonequilibrium<br />

is important to correctly characterise the flow field about the vehicle. On a more practical note,<br />

the correct modelling <strong>of</strong> nonequilibrium phenomena is required for accurate estimates <strong>of</strong> heat<br />

loading on the vehicle surface. Sutton and Gn<strong>of</strong>fo [114] have reported that a little more than<br />

half <strong>of</strong> the stagnation point heating rate for entry into air at 10.9 km/s is due to recombina-<br />

tion <strong>of</strong> atomic species <strong>of</strong> O and N. This effect on heat transfer estimates can only be reliably<br />

modelled by including finite-rate chemistry effects.<br />

The influence <strong>of</strong> chemical nonequilibrium phenomena in gas dynamics is not limited to<br />

blunt body flows. Its influence extends to combustion processes, detonation waves and nozzle<br />

flows to name a few examples and the same basic theoretical treatment can be applied to each<br />

<strong>of</strong> theses types <strong>of</strong> flows.<br />

In this chapter, a computational model for calculating the finite-rate chemical evolution <strong>of</strong><br />

reacting gas in nonequilibrium flows is described. In essence this chapter is dedicated to the<br />

term<br />

˙ω<br />

as it appears in Equation 2.2; its theory, implementation, verification and validation is reported.<br />

The theory behind the coding implementation is presented in two sections: the model for a<br />

mixture <strong>of</strong> thermally perfect gases is presented in Section 4.1 and the model for the chemical<br />

kinetics is described in Section 4.2. The numerical methods for solving the chemical kinetic rate<br />

equation are presented in Section 4.2.3. An <strong>of</strong>t encountered problem in the numerical solution<br />

<strong>of</strong> the chemical rate equations is that numerical inaccuracies can lead to problems ensuring<br />

that mass is conserved in the system. In Section 4.3, an original treatment — to the best <strong>of</strong> my<br />

knowledge — to the numerical solution <strong>of</strong> the chemical kinetics equations is presented; this<br />

method directly addresses the problems <strong>of</strong> mass conservation. The implementation is verified<br />

by comparison with an analytical solution to a hydrogen-iodine system in Section 4.4, and,<br />

finally, some validation cases for gas dynamic flows in chemical nonequilibrium are shown in<br />

Section 4.5.<br />

gas.<br />

1 This is a result <strong>of</strong> shock processing, or consider this a result <strong>of</strong> indirect transferal <strong>of</strong> vehicle kinetic energy to the

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

Saved successfully!

Ooh no, something went wrong!