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dc.contributor.author | Iovleva O. | |
dc.contributor.author | Larionov V. | |
dc.date.accessioned | 2018-09-18T20:17:58Z | |
dc.date.available | 2018-09-18T20:17:58Z | |
dc.date.issued | 2007 | |
dc.identifier.issn | 1068-7998 | |
dc.identifier.uri | https://dspace.kpfu.ru/xmlui/handle/net/138454 | |
dc.description.abstract | The theoretical study of vibration combustion using a model of the pulsejet engine was carried out. The frequencies and amplitudes of gas vibrations that were calculated by the energy method are well agreed with experimental data. © Allerton Press, Inc. 2007. | |
dc.relation.ispartofseries | Russian Aeronautics | |
dc.title | A mathematical model of vibration combustion in a tube with sudden cross-section change | |
dc.type | Article | |
dc.relation.ispartofseries-issue | 3 | |
dc.relation.ispartofseries-volume | 50 | |
dc.collection | Публикации сотрудников КФУ | |
dc.relation.startpage | 303 | |
dc.source.id | SCOPUS10687998-2007-50-3-SID36448938310 |