Validation of the model of hybrid detonation of hydrogen-air mixtures with aluminium particles
Čelâbinskij fiziko-matematičeskij žurnal, Tome 9 (2024) no. 2, pp. 177-186.

Voir la notice de l'article provenant de la source Math-Net.Ru

Verification and validation of the model of the reduced kinetics of hybrid detonation in hydrogen-air mixtures with fine aluminum particles was carried out. The formula of integral heat release is obtained depending on the fuel excess coefficient for poor hydrogen-air mixtures. The results are consistent with experimental data on the detonation rate. The constants of the aluminum combustion reactions are determined, which ensure the coordination of the detonation rate in air suspensions of aluminum particles. The processes of gas detonation in hydrogen-air mixtures and hybrid detonation with aluminum particles are numerically modeled. The dependencies of the hybrid detonation rate on the particle concentration are consistent with the known data. The comparison with experiments on cellular gas and hybrid detonation patterns is carried out: the degree of regularity, the size of the cells, the slope of the trajectories of triple points.
Keywords: physical and mathematical modeling, numerical modeling, hydrogen-air mixtures, aluminum particles, hybrid detonation.
@article{CHFMJ_2024_9_2_a1,
     author = {A. A. Afanasenkov and T. A. Khmel},
     title = {Validation of the model of hybrid detonation of hydrogen-air mixtures with aluminium particles},
     journal = {\v{C}el\^abinskij fiziko-matemati\v{c}eskij \v{z}urnal},
     pages = {177--186},
     publisher = {mathdoc},
     volume = {9},
     number = {2},
     year = {2024},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/CHFMJ_2024_9_2_a1/}
}
TY  - JOUR
AU  - A. A. Afanasenkov
AU  - T. A. Khmel
TI  - Validation of the model of hybrid detonation of hydrogen-air mixtures with aluminium particles
JO  - Čelâbinskij fiziko-matematičeskij žurnal
PY  - 2024
SP  - 177
EP  - 186
VL  - 9
IS  - 2
PB  - mathdoc
UR  - http://geodesic.mathdoc.fr/item/CHFMJ_2024_9_2_a1/
LA  - ru
ID  - CHFMJ_2024_9_2_a1
ER  - 
%0 Journal Article
%A A. A. Afanasenkov
%A T. A. Khmel
%T Validation of the model of hybrid detonation of hydrogen-air mixtures with aluminium particles
%J Čelâbinskij fiziko-matematičeskij žurnal
%D 2024
%P 177-186
%V 9
%N 2
%I mathdoc
%U http://geodesic.mathdoc.fr/item/CHFMJ_2024_9_2_a1/
%G ru
%F CHFMJ_2024_9_2_a1
A. A. Afanasenkov; T. A. Khmel. Validation of the model of hybrid detonation of hydrogen-air mixtures with aluminium particles. Čelâbinskij fiziko-matematičeskij žurnal, Tome 9 (2024) no. 2, pp. 177-186. http://geodesic.mathdoc.fr/item/CHFMJ_2024_9_2_a1/

[1] Khasainov A., Veyssiere B., “Steady, plane, double-front detonations in gaseous detonable mixtures containing a suspension of aluminum particles”, Dynamics of Explosions, AIAA, 1988, 284–299

[2] Veyssiere B., Ingignoli W., “Existence of the detonation cellular structure in two-phase hybrid mixtures”, Shock Waves, 12:4 (2003), 291–299 | DOI

[3] Veyssiere B., Khasainov B. A., “A model for steady, plane, double-front detonations (DFD) in gaseous explosive mixtures with aluminum particles in suspension”, Combustion and Flame, 85:1–2 (1991), 241–253 | DOI

[4] Veyssiere B., Khasainov B. A., “Structure and multiplicity of detonation regimes in heterogeneous hybrid mixtures”, Shock Waves, 4:4 (1995), 171–186 | DOI

[5] Khasainov B. A., Veyssiere B., “Initiation of detonation regimes in hybrid two-phase mixtures”, Shock Waves, 5:1 (1996), 9–15 | DOI

[6] Khmel T. A., Lavruk S. A., “Development of a model of hybrid detonation in a mixture of oxygen–hydrogen–argon with aluminum particles”, Combustion and Explosion, 16:1 (2023), 63–69 | MR

[7] Khmel T.A., Lavruk S.A., Afanasenkov A.A., “Propagation of hybrid detonation in a hydrogen-oxygen mixture with aluminum particles in a channel with expansion”, Chelyabinsk Physical and Mathematical Journal, 8:3 (2023), 371–386 | DOI | MR

[8] Khmel T.A., Lavruk S.A., “Structure and propagation of Chapman — Jouget waves in a hydrogen-oxygen mixture with aluminum particles”, Chelyabinsk Physical and Mathematical Journal, 8:4 (2023), 583–590 | MR

[9] Bedarev I.A., Rylova K.V., Fedorov A.V., “Application of detailed and reduced kinetic schemes for the description of detonation of diluted hydrogen-air mixtures”, Combustion, Explosion and Shock Waves, 51:5 (2015), 528–539 | DOI

[10] Bedarev I. A., Temerbekov V. M., “Estimation of the energy of detonation initiation in a hydrogen-oxygen mixture by a high velocity projectile”, Thermal Science, 25 (2021), 3889–3897 | DOI

[11] Bedarev I. A., Temerbekov V. M., “Modeling of attenuation and suppression of cellular detonation in the hydrogen-air mixture by circular obstacles”, International Journal of Hydrogen Energy, 47 (2022), 38455–38467 | DOI | MR

[12] Ciccarelli G., Ginsberg T., Boccio J., Economos C., Sato K., Kinoshita M., “Detonation cell size measurements and predictions in hydrogen-air-steam mixtures at elevated temperatures”, Combustion and Flame, 99 (1994), 212–220 | DOI

[13] Vasil’ev V.M., Vol’pert A.I., Klychnikov L.V., Petrov Y.M., Salakatova L.S., Stesik L.N., “Calculation of fuel-air mixture detonation parameters”, Combustion, Explosion and Shock Waves, 16:3 (1980), 354–356 | DOI

[14] Khmel T.A., Lavruk S.A., “Modeling of cellular detonation in gas suspensions of submicron aluminum particles with different distributions of concentration”, Combustion, Explosion and Shock Waves, 58:3 (2022), 253–268 | DOI | DOI | Zbl

[15] Khmel T.A., Lavruk S.A., “Modeling of cellular detonation in gas suspensions of two fractions of aluminum nanoparticles”, Combustion, Explosion and Shock Waves, 56:2 (2020), 188–197 | DOI

[16] Hosoda H., Hayashi A. K., Yamada E., “Numerical analysis on combustion characteristics of nano aluiminum particle-oxygen Two-Phase detonation”, Science and Technology of Energetic Materials, 74 (2013), 34–40

[17] Benedick W. B., Knystautas R., Lee J. H. S., “Large-scale experiments on the transmission of fuel-air detonations from two-dimensional channels”, Progress in Astronautics and Aeronautics, 94 (1984), 546–555