Simulation of Turbulent Mixing Behind a Strut Injector in Supersonic Flow
The flowfield downstream of a strut-based injection system in a supersonic combustion ramjet is investigated using large-eddy simulation with a new localized dynamic subgrid closure for compressible turbulent mixing. Recirculations are formed at the base of the strut in the nonreacting flow and trap...
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Published in | AIAA Journal Vol. 48; no. 3; pp. 526 - 539 |
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Main Authors | , |
Format | Journal Article |
Language | English Japanese |
Published |
Virginia
American Institute of Aeronautics and Astronautics (AIAA)
01.03.2010
American Institute of Aeronautics and Astronautics |
Subjects | |
Online Access | Get more information |
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