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dc.contributor.author | Avkhadiev F. | |
dc.contributor.author | Elizarov A. | |
dc.date.accessioned | 2018-09-17T21:33:32Z | |
dc.date.available | 2018-09-17T21:33:32Z | |
dc.date.issued | 2001 | |
dc.identifier.issn | 1446-1811 | |
dc.identifier.uri | https://dspace.kpfu.ru/xmlui/handle/net/135147 | |
dc.description.abstract | A problem of estimation of the critical Mach number for a class of carrying wing profiles with a fixed theoretical angle of attack is considered. The Chaplygin gas model is used to calculate the velocity field of the flow. The original problem is reduced to a special minimax problem. A solution is constructed for an extended class of flows including multivalent ones, hence M* is estimated from above. For a fixed interval [0, β0], β0 ≃ 3π/8, an estimate of M* is given from below. © Australian Mathematical Society 2001,. | |
dc.relation.ispartofseries | ANZIAM Journal | |
dc.title | Bilateral estimates of the critical mach number for some classes of carrying wing profiles | |
dc.type | Article | |
dc.relation.ispartofseries-issue | 4 | |
dc.relation.ispartofseries-volume | 42 | |
dc.collection | Публикации сотрудников КФУ | |
dc.relation.startpage | 494 | |
dc.source.id | SCOPUS14461811-2001-42-4-SID33747272333 |