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 |
|