Abstract:
Studies have been made of the structure
of weak compression (shock) waves in relaxing
gases. These studies have been primarily concerned
with the development of separate theoretical
and experimental techniques. These techniques
are not inter-related in general except in the
overall context of Vibrational relaxation.
The theoretical studies have been concerned
with the influence on the structure of weak normal
shock waves of translational non-equilibrium.
bimodal relaxation and second order unimodal
relaxation. The affect of translational nonequilibrium
on the relaxation process has been
studied by forming an asymptotic expansion in the
ratio of the viscous length to the relaxation
length. The perturbation scheme was singular and
required the application at the method of matched
asymptotic expansions. Bimodal relaxation has
been studied by forming an asymptotic expansion
in the ratio of the energy of the secondary
vibrational mode to the total Vibrational energy.
The addition of a second order term to
the rate equation describing the behaviour of a
single vibrational mode has also been studied by
forming an asymptotic expansion. In this case.
the perturbation parameter was the ratio of the
two relaxation times concerned.
The experimental studies have been
concerned with the production and study or weak
normal shock waves in the Cranfield Institute or
Technology 2" shock tube. A time resolved
quantitative schlieren system has been used for
the study of the weak normal shock waves. This
particular system had been developed previously
for this purpose. and further developments and
refinements have been made to it.
Experimental studies have been made with
the schlieren system of the structure or strong
incident shock waves in carbon dioxide. The
vibrational relaxation time of carbon dioxide
determined in this way for translational
temperatures from 300 o K to 1200 o K has been found
to be in reasonable agreement with measurements
made elsewhere.
A technique has been developed for the
production of weak incident shock waves in t.i.1e
shock tube, which involved the positioning of a
perforated plate in the channel of the shock tube.
The vibrational relaxation time of carbon dioxide
determined in this way for translational
o
temperatures of approximately 300 K has been found
to be in good agreement with measurements made
elsewhere. Good agreement has also been obtained
between the experimentally measured density
gradient profiles and theoretical profiles. The
curvature of the shock waves obscured the transition
from a fully dispersed to a partly dispersed shook
wave.
Further improvements and refinements have
been made to a technique which had been developed
previously for the propagation of weak normal
shock waves through the reflected shock region
of the shock tube flow. This technique was used
to study the behaviour of fully dispersed shock
waves at high temperatures. The relaxation time
of carbon dioxide determined in this way for
temperatures from 300 o K to 600o K has been found
to be in good agreement with measurements made
elsewhere.