RUS  ENG
Full version
JOURNALS // Teplofizika vysokikh temperatur // Archive

TVT, 2019 Volume 57, Issue 4, Pages 560–571 (Mi tvt11172)

This article is cited in 8 papers

Heat and Mass Transfer and Physical Gasdynamics

Modeling of detonation of metal-gas combustible mixtures in high-speed flow behind a shock wave

V. Yu. Gidaspov, N. S. Severina

Moscow Aviation Institute (National Research University)

Abstract: A physical and mathematical model that makes it possible to describe the processes of the self-ignition, combustion, and detonation of combustible metal-gas mixtures is given. A simplified physical and mathematical model of the process has been developed. Dispersed particles are considered to be multicomponent, and the processes of the melting and evaporation of the particle material, as well as surface reactions (in which both liquid and gaseous components can participate) are taken into account. The carrier gas is considered multicomponent with the possibility of an arbitrary number of chemical reactions. The case in which the combustion products are in a state of thermodynamic equilibrium is considered, and the presence of fine particles of metals, oxides, and metal nitrides are taken into account. The structure and minimum propagation velocity of a stationary detonation wave are determined by calculation. It is shown that the parameters calculated in waves asymptotically tend to their equilibrium values. The developed physical and mathematical model and computational algorithms can be used to create methods to model the combustion and detonation of metal-gas mixtures in a multidimensional formulation.

UDC: 533.6

Received: 28.01.2019
Revised: 28.02.2019
Accepted: 27.03.2019

DOI: 10.1134/S0040364419040069


 English version:
High Temperature, 2019, 57:4, 514–524

Bibliographic databases:


© Steklov Math. Inst. of RAS, 2024