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Numerical Simulation of Viscous Perfect Gas Dynamics (Paperback)
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Numerical Simulation of Viscous Perfect Gas Dynamics (Paperback)
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The monograph summarizes the results of research of many years in
the field of numerical simulation based on the continuum dynamics
equations for transonic and supersonic flows of viscous perfect gas
in the context of the problems of external aerodynamics, which have
been obtained by the authors and their colleagues and published in
different domestic journals. The monograph consists of two parts.
The first part deals with stationary and non-stationary
two-dimensional problems, stationary three-dimensional problems are
considered in the second part. That said, the uniform steady flow
over the bodies of comparably simple configuration, which surface
is determined analytically, is studied. Each part begins with
mathematical statement of the problem and method of its numerical
analysis. This is followed by the detailed discussion of the
results of computations for a number of aerodynamic problems, which
have been obtained within some range of the key similarity
parameters. The problems under consideration are divided into two
groups according to the purposes. The problems intended to the
theoretical study of the flow field near the streamlined body, its
local and total aerodynamic characteristics and of the effect of
the key similarity parameters on the flow field characteristics
refer to the first group. For this purpose it is necessary to
obtain computational results within a wide range of the key
similarity parameters. Such research is usually performed using the
bodies of simple configuration, with the great attention being paid
to the verification of the numerical simulation method and adequacy
of the results. The monograph considers the classic bodies such as:
circular and elliptical cylinders, sharp circular and elliptical
cones. The problems related to the computational validation of the
aerodynamic experiment in different supersonic and hypersonic wind
tunnels of TsAGI refer to the second group. In this case the
computations are implemented for the considered body as applied to
the experimental conditions. That said, in most cases the
computations include estimation of the flow field along the whole
channel of the wind tunnel, i.e. the flow of the actuating medium
is calculated in the nozzle and in the test chamber of the wind
tunnel both with and without the model in it. The results of
computations are compared with the experimental data. The monograph
considers mainly the axisymmetric blunted bodies of Martian probe
type (United States and European analogs). The monograph is of
interest for professionals in the field of computational and
applied aerodynamics as well as for undergraduate and graduate
students whose major is somehow related to the applied
aerodynamics.
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