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...

Full description

Saved in:
Bibliographic Details
Published inAIAA Journal Vol. 48; no. 3; pp. 526 - 539
Main Authors Génin, Franklin, Menon, Suresh
Format Journal Article
LanguageEnglish
Japanese
Published Virginia American Institute of Aeronautics and Astronautics (AIAA) 01.03.2010
American Institute of Aeronautics and Astronautics
Subjects
Online AccessGet more information

Cover

Loading…