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. Investigations are performed for regions of the incoming supersonic flow, inside of the scramjet channel, and outside of it. Dependences of the total aerodynamic force projection onto the direction of scramjet motion on its speed and mass fuel supply rate are analyzed.
| Original language | English |
|---|---|
| Pages (from-to) | 908-913 |
| Number of pages | 6 |
| Journal | Russian Physics Journal |
| Volume | 56 |
| Issue number | 8 |
| DOIs | |
| Publication status | Published - 2013 |
| Externally published | Yes |
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Keywords
- combustion
- gas dynamic processes
- mathematical modeling
- scramjet
- total aerodynamic force
ASJC Scopus subject areas
- Physics and Astronomy(all)
Cite this
Modeling of the Process of Motion of a Scramjet in the Atmosphere. / Vasenin, I. M.; Shrager, É R.; Glazunov, A. A.; Krainov, A. Yu; Krainov, D. A.
In: Russian Physics Journal, Vol. 56, No. 8, 2013, p. 908-913.Research output: Contribution to journal › Article
}
TY - JOUR
T1 - Modeling of the Process of Motion of a Scramjet in the Atmosphere
AU - Vasenin, I. M.
AU - Shrager, É R.
AU - Glazunov, A. A.
AU - Krainov, A. Yu
AU - Krainov, D. A.
PY - 2013
Y1 - 2013
N2 - 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. Investigations are performed for regions of the incoming supersonic flow, inside of the scramjet channel, and outside of it. Dependences of the total aerodynamic force projection onto the direction of scramjet motion on its speed and mass fuel supply rate are analyzed.
AB - 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. Investigations are performed for regions of the incoming supersonic flow, inside of the scramjet channel, and outside of it. Dependences of the total aerodynamic force projection onto the direction of scramjet motion on its speed and mass fuel supply rate are analyzed.
KW - combustion
KW - gas dynamic processes
KW - mathematical modeling
KW - scramjet
KW - total aerodynamic force
UR - http://www.scopus.com/inward/record.url?scp=84899425754&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84899425754&partnerID=8YFLogxK
U2 - 10.1007/s11182-013-0117-2
DO - 10.1007/s11182-013-0117-2
M3 - Article
AN - SCOPUS:84899425754
VL - 56
SP - 908
EP - 913
JO - Russian Physics Journal
JF - Russian Physics Journal
SN - 1064-8887
IS - 8
ER -