Low emissions and high efficiencies
can be realized in combustion
systems that operate at high-pressure and low-temperature conditions
(high densities). The design of such engines relies on accurate models
of the physical processes involved. Under these conditions, the ideal
gas model widely used in computational fluid dynamics (CFD) simulations
fails to properly capture the relation among pressure, density, and
temperature as well as inter-relations among other thermodynamic and
transport properties. As such, discrepancies between experimental
observations and CFD simulations cannot only be traced to uncertainties
from experiments, turbulent, or combustion models. This paper offers
a possible solution to the implementation of the real gas equation
of state models in combustion simulations. The large number of species
in combustion simulations requires effort to provide the relevant
real gas properties. A method is suggested for incorporating these
properties in simulations based on available transport and thermodynamic
data of chemical kinetic models. This attempt also brings out an often-ignored
problem in existing chemical kinetic models in the literature, namely,
the nonsystematic assignment of transport properties for various species.
To clearly demonstrate the need for real gas models in reacting flows,
simulations are carried out of a high-pressure
n
-heptane
jet into a quiescent chamber of air based on ideal gas and real gas
models. The defects of the ideal gas model are revealed, and the proposed
method of property estimation is justified as a convenient solution.