23 research outputs found

    Diffusion coefficient when fine aerosol media propagate in a confined volume

    Get PDF
    An experimental estimation is reported of the value of the effective diffusion coefficient during aerosol deposition in a confined volume. Aerosol propagation regularities have experimentally been studied in a chamber of a complex configuration with different placement of aerosol generators

    Morphology of ceramic particles produced by plasma-chemical synthesis

    Get PDF
    Thermal and diffusion processes in the droplet weakly concentrated metal salt solution during its heating in the plasma chemical reactor, in order to synthesize metal oxide powders are considered. Numerical study is based on previously proposed physical-mathematical model. The results of numerical calculations are analyzed to assess the possible influence of the operation parameters of the reactor and the characteristics of the initial solution (precursor) on the morphology of the particles formed

    Investigation of working processes in a flowing channel of ramjet engine

    Get PDF
    The technique and results of experimental-theoretical study of gas-dynamics, heat transfer and the structure of gas-flow in the flowing channel of a ramjet engine in Mach number range M = (5-7) are presented. The temperature distribution along the flowing channel of a ramjet engine was experimentally obtained. The temperature along the wall of the flowing channel of the axisymmetric model was measured using the developed thermoprobe. Distributions of Mach number and temperature along the symmetry axis of the flowing channel of the model are obtained numerically. Comparison of the numerical and experimentally obtained values of the Mach number showed their qualitative agreement

    Experimental study of flow around axisymmetric bodies in supersonic flow in case of a local injection into the boundary layer

    Get PDF
    A technique of experimental determination of the parameters and structure of supersonic air flow around of axisymmetric bodies form in the range of Mach numbers M = (2 Γ· 5) are presented. The results of the investigation of the interaction a supersonic stream flowing around of an axisymmetric model with gas jet which inject into the boundary layer are given

    Mathematical modelling of the liquid atomization process by cocurrent gas flow

    Get PDF
    This paper focuses on the physical-mathematical model of liquid atomization in the spray pattern of an ejection nozzle. A flow field of a gas phase behind the nozzle section is computed using the Ansys Fluent package. Dynamics of molten metal droplets in the gas phase within a trajectory approach is calculated. Using the presented model, numerical calculation results are given

    Dynamics and heat and mass transfer of liquid-droplet cloud in the emergency discharge of aviation fuel into the atmosphere

    No full text
    A mathematical model for the propagation of liquid-droplet cloud in the atmosphere during the emergency discharge of aviation fuel is presented. The results of a numerical analysis of the dynamics and heat and mass transfer of a liquid-droplet cloud in the emergency discharge of aviation fuel into the atmosphere, depending on the season-climatic and meteorological conditions of specific regions of Russia are given

    Experimental Research of Supersonic Flow Around Simulating Rocket-Ramjet

    No full text
    The results of experimental researches of the structure and of the basic parameters of the air when flow around flat and axisymmetric models of rocket-ramjet engine are presented

    Experimental Research of Supersonic Flow Around Simulating Rocket-Ramjet

    Get PDF
    The results of experimental researches of the structure and of the basic parameters of the air when flow around flat and axisymmetric models of rocket-ramjet engine are presented

    Experimental research of supersonic flow around simulating rocket-ramjet

    No full text
    The results of experimental researches of the structure and of the basic parameters of the air when flow around flat and axisymmetric models of rocket-ramjet engine are presente

    Heat and mass transfer in a high-porous low-temperature thermal insulation in real operating conditions

    No full text
    The results of numerical simulation of heat and mass transfer in a high-porous low-temperature insulation in conditions of insulation freezing, a moisture migration to the front of phase transition and a condensation forming on an outer contour of interaction were obtained. Values of heat leakage were established
    corecore