Abstract
| Language | English |
|---|---|
| Pages | 2801-2813 |
| Number of pages | 13 |
| Publication status | Published - 24 Sep 2010 |
| Event | 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010 - Nice, France Duration: 19 Sep 2010 → 24 Sep 2010 |
Conference
| Conference | 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010 |
|---|---|
| Abbreviated title | ICAS 2010 |
| Country | France |
| City | Nice |
| Period | 19/09/10 → 24/09/10 |
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Keywords
- supersonic aerodynamics
- computational results
- implicit large eddy simulation
- high-resolution methods
- jet mixing
- jet penetration
- numerical scheme
- scramjet combustors
Cite this
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Investigation of sonic jet mixing in a stream of supersonic cross-flow using large eddy simulations. / Rana, Z.A.; Drikakis, D.; Thornber, B.J.
2010. 2801-2813 Paper presented at 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010, Nice, France.Research output: Contribution to conference › Paper
TY - CONF
T1 - Investigation of sonic jet mixing in a stream of supersonic cross-flow using large eddy simulations
AU - Rana, Z.A.
AU - Drikakis, D.
AU - Thornber, B.J.
PY - 2010/9/24
Y1 - 2010/9/24
N2 - This paper presents an application of a finite volume Godunov-type implicit large eddy simulation (ILES) method to study a transverse sonic Jet Injection into a Supersonic Cross-flow (JISC) of turbulent flow. The ILES method is based on fifth-order in space and third-order in time numerical schemes along with a digital-filter-based turbulent inflow data generation method. The simulations are compared against experimental data and other computational results obtained from classical LES methods. Using the simulation results, the jet penetration and flow properties upstream and downstream the jet plume are investigated.
AB - This paper presents an application of a finite volume Godunov-type implicit large eddy simulation (ILES) method to study a transverse sonic Jet Injection into a Supersonic Cross-flow (JISC) of turbulent flow. The ILES method is based on fifth-order in space and third-order in time numerical schemes along with a digital-filter-based turbulent inflow data generation method. The simulations are compared against experimental data and other computational results obtained from classical LES methods. Using the simulation results, the jet penetration and flow properties upstream and downstream the jet plume are investigated.
KW - supersonic aerodynamics
KW - computational results
KW - implicit large eddy simulation
KW - high-resolution methods
KW - jet mixing
KW - jet penetration
KW - numerical scheme
KW - scramjet combustors
UR - http://www.scopus.com/inward/record.url?eid=2-s2.0-84878487883&partnerID=40&md5=b5de475d9540e5fc2e834fdb5797ee6a
M3 - Paper
SP - 2801
EP - 2813
ER -