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  • FORMATION OF THE ATMOSPHERIC ELECTRODE LAYER STRUCTURE

    S.S. Svidelsky, V.S. Litvinova, G. V. Kupovykh, A. G. Klovo
    2021-01-19
    Abstract ▼

    The problem of the formation of the electric state in the lower layer of the atmosphere near
    the Earth's surface is considered in the article. An electrodynamic model of a non-stationary turbulent-
    convective surface layer is investigated in the approximation of the electrode effect. The
    initial system consists of the ionization-recombination equations for aeroions and the Poisson
    equation. Depending on the meteorological conditions in the atmosphere, the cases of classical
    and turbulent electrode effects, as well as the approximation of strong turbulent mixing, are considered
    separately. Turbulent and convective transport, the degree of air ionization, and the presence
    of submicron aerosol particles in the air are factors that affect the space-time structure of the
    electrode layer. Dimensionless parameters (similarity criteria) for electrodynamic equations are
    revealed, which allow choosing the appropriate approximation for modeling the structure of the
    electrode layer depending on atmospheric conditions. In an aerosol-free atmosphere, the time to
    establish a stationary state in the electrode layer is about 5 minutes, for the classical layer (the
    typical height is about 4-5 m), and in the turbulent layer-about 15 minutes. (the typical height is
    about 10 m). In the case of strong turbulent mixing, the distribution scale of electrical quantities
    increases to hundreds of meters. The ratio of the characteristic velocities of turbulent and convective
    processes indicates the predominant physical mechanism of ion transport and the formation of
    the electrode layer structure. An increase in the rate of convective transport directed downwards
    leads to a weakening of the turbulent mixing mechanism, and when moving up, the opposite effect
    occurs. The presence of a submicron aerosol in the atmosphere leads to the formation of heavy
    ions, the mobility of which is much less than that of aeroions. Single-charged aerosol particles
    with a concentration not exceeding the number of aeroions slightly change the spatiotemporal
    characteristics of the electrode layer. While the presence of repeatedly charged aerosol particles
    in the surface air increases the time of electrical relaxation and reduces the height of the electrode
    layer. At sufficiently high concentrations of aerosol (more than the number of aeroions by an order
    of magnitude or more), it is necessary to take into account its transport by turbulentconvective
    flows, and the structure of the electrode layer is determined only by heavy ions.

  • MULTIPHYSICS SIMULATION IN ANSYS CFX AND SYSTEM COUPLING OF HEAT TRANSFER INSIDE HERMRTIC CASE OF STRAPDOWN INERTIAL NAVIGATION SYSTEM

    А.А. Medeltsev, P. А. Shapovalov, М. V. Voronov, А. I. Polukhina, P.N. Sigaleva, А.V. Frolov
    2022-04-21
    Abstract ▼

    The article presents a numerical simulation of non-stationary convective-conductive heat
    transfer of the strapdown inertial navigation system (SINS), developed in the JSC «CNIIAG».
    The numerical simulation is carried out in the ANSYS Mechanical. The aim of the study is a comprehensive
    analysis of heat exchange processes, which are characteristic to the device operation,
    including mutual spatial influence of thermal powers on each other, as well as on the block of
    sensitive elements. The simulation of heat transfer inside the hermetic case of the SINS is carried out for critical operating conditions in a strongly and weakly coupled consideration with a comparison
    of both approaches. ANSYS Mechanical, CFX and System Coupling simulation modules
    are chosen for program implementation of each approach. The k-e model of air turbulence with
    implicit consideration of the effect in the boundary layers and diffusion correction in shear flows is
    chosen for this approach. External heat exchange with ambient air is considered by setting convective
    boundary conditions on the external surfaces of the SINS, considering their orientation.
    To obtain numerical values of the heat transfer coefficients, the orientation of each surface in
    space is taken into account by using the appropriate coefficient. The presence of irregularities on
    the surfaces of the SINS in the contacts between solid components is considered by using the calculation
    of thermal resistances of the actual contact and intercontact layer. The simulation results
    of deformed state of SINS structural system, resulting from the action of a non-symmetric thermal
    field, is presented. The analysis of the obtained graphs is carried out. Stiffness indicators of the
    SINS structural system is defined as angles of deviation of sensitivity axes caused by thermal deformations.
    The obtained results make it possible to evaluate the engineering solutions for the
    quality of heat removal from the elements of the PCBs, bypassing the sensitive elements of the
    device, adopted at the stage of product layout.

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