Nonequilibrium in high enthalpy carbon dioxide flows
Abstract
A study of high enthalpy nonequilibrium flows of carbon
dioxide is presented.
Chemical and thermodynamic models are obtained for
nozzle and model flows. A numerical survey of high enthalpy
carbon dioxide nozzle expansions shows that the assumption of
vibrational equilibrium is a good one, and that ionization is
energetically insignificant up to a reservoir specific enthalpy
of 3.3 x 10¹¹ cm² s⁻². It also shows that the reservoir
entropy correlation observed to hold for air by Warren and
Harris (1964) applies to carbon dioxide expansions. A numerical
survey of wedge flows shows that over a large range of conditions
vibrational relaxation of C0₂ and CO is slow enough to be
an important nonequilibrium process in flows or laboratory
scale. The effect of translational nonequilibrium between the
electrons and heavy particles is significant in blunt body
flows at high enthalpies. Experimentally, the importance of various nonequilibrium
processes is examined under different flow situations. The
measurements of nozzle flow variables show good agreement with
predictions. Single wavelength interferometry is used to
observe the complete flow fields of wedges and blunt bodies.
The channelled spectra technique is used to measure the electron
and heavy particle densities in the shock layer of a blunt body.
Estimates of electron densities are consistent with predictions.
The hook method is used to estimate the impurity levels. It
is shown that these impurities have a negligible effect on the
electron densities measured. The dissociation rate of undiluted carbon dioxide is
measured in the temperature range 2500-7000 K and compared
with those by other workers. An activation energy of 104
Kcal/mole from these measurements is in agreement with some
recently reported measurements. Studies of normal shock
waves in the velocity range 3 to 17.3 Km/s show that above a
velocity of 11 Km/s, the thermodynamic model of carbon dioxide
used in equilibrium calculations is inadequate and that above
13 Km/s, significant radiation losses can be expected.
Instabilities are observed in the shock heated gas
slug behind a normal shock wave, for various shock tube and
driver conditions, and an empirical stability correlation is
obtained from these conditions.
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