Stability of composite solid propellant ignition by a local source of limited energy capacity; Combustion, Explosion, and Shock Waves; Vol. 50, iss. 6
| Parent link: | Combustion, Explosion, and Shock Waves.— , 1965- Vol. 50, iss. 6.— 2014.— [P. 670-675] |
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| Muut tekijät: | , |
| Yhteenveto: | Title screen A numerical simulation of solid-phase ignition of a composite propellant by a single small disk-shaped metal particle heated to a high temperature is performed. In the “heat flux amplitude-ignition delay ” coordinates, an region of stable initiation of combustion of a typical composite solid propellant under local heating by a source of limited energy capacity is selected. The limiting amplitudes of heat fluxes during ignition of the condensed substance under conductive and radiative heating are compared. Режим доступа: по договору с организацией-держателем ресурса |
| Kieli: | englanti |
| Julkaistu: |
2014
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| Linkit: | http://dx.doi.org/10.1134/S0010508214060082 |
| Aineistotyyppi: | Elektroninen Kirjan osa |
| KOHA link: | https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=649442 |
| Yhteenveto: | Title screen A numerical simulation of solid-phase ignition of a composite propellant by a single small disk-shaped metal particle heated to a high temperature is performed. In the “heat flux amplitude-ignition delay ” coordinates, an region of stable initiation of combustion of a typical composite solid propellant under local heating by a source of limited energy capacity is selected. The limiting amplitudes of heat fluxes during ignition of the condensed substance under conductive and radiative heating are compared. Режим доступа: по договору с организацией-держателем ресурса |
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| DOI: | 10.1134/S0010508214060082 |