Modelling of internal ballistics processes in scramjet engine during the motion in the atmosphere
| dc.contributor.author | Vasenin, I.M. | |
| dc.contributor.author | Shrager, É.R. | |
| dc.contributor.author | Krainov, A.Yu. | |
| dc.contributor.author | Krainov, D.A. | |
| dc.date.accessioned | 2019-05-20T11:38:39Z | |
| dc.date.available | 2019-05-20T11:38:39Z | |
| dc.date.issued | 2015-12-23 | |
| dc.description.abstract | Physical and mathematical model and results of modeling of the processes proceeding in the channel of a scramjet and in the surrounding atmosphere are presented for Mach numbers of 6.7–10. The mathematical model is based on the gas dynamics equations written in the two-dimensional approximation taking into account combustion of a gaseous fuel. Dependences of the total aerodynamic force projection onto the direction of scramjet motion on its speed and mass fuel supply rate are analyzed. | ru_RU |
| dc.identifier.citation | Vasenin, I.M. Modelling of internal ballistics processes in scramjet engine during the motion in the atmosphere / I.M. Vasenin, É.R. Shrager, A.Yu. Krainov [et al.] // Eurasian Physical Technical Journal. – 2015. – Vol.12. – № 2(24). – P. 60-64. | ru_RU |
| dc.identifier.issn | 2413-2179 | |
| dc.identifier.issn | 1811-1165 | |
| dc.identifier.uri | https://rep.buketov.edu.kz//handle/data/5956 | |
| dc.language.iso | en | ru_RU |
| dc.publisher | Publishing House of the KarSU named after E.A.Buketov | ru_RU |
| dc.relation.ispartofseries | Eurasian Physical Technical Journal;Vol.12, № 2(24) | |
| dc.subject | scramjet | ru_RU |
| dc.subject | gas dynamic processes | ru_RU |
| dc.subject | gaseous fuel | ru_RU |
| dc.subject | combustion | ru_RU |
| dc.subject | total aerodynamic force | ru_RU |
| dc.subject | mathematical modeling | ru_RU |
| dc.title | Modelling of internal ballistics processes in scramjet engine during the motion in the atmosphere | ru_RU |
| dc.type | Article | ru_RU |