RESEARCH OF EXTERNAL HEAT SHOCK PROCESSES FOR PYROTECHNIC METAL OXIDE PRODUCTS IN CONDITIONS OF SHOOTING AND FLIGHT
Abstract
A mathematical model of external thermal shock actions of supersonic air flow on metal shells of charges of pyrotechnic mixtures of magnesium and aluminum powders and metal oxides, taking into account the temperature dependences of their thermophysical properties and allows with a relative error of 7… 9% to calculate distributions heat flow from the boundary layer along the surface of the shells and the temperature of them thickness has been developed.
A scientifically sound method for determining critical parameters shock thermody (velocities of air flow, time of its action, Reynolds criterion, which characterizes the flow regime (laminar, turbulent)), controlling which by adjusting the technological parameters (ratio and dispersion of components, compaction coefficient, charge diameter and material shell) can prevent premature fire and explosion destruction of products in terms of their launches has been developed.