Large-eddy simulation of a supersonic jet using high-order flux reconstruction scheme

Takanori Haga, Seiji Tsutsumi, Soshi Kawai, Ryoji Takaki

Research output: Chapter in Book/Report/Conference proceedingConference contribution

8 Citations (Scopus)


Large-eddy simulations of an ideally expanded supersonic jet at Mach number 1.8 are performed by a high-order unstructured grid solver for aiming at the validation for aero-acoustic applications. The developed solver is based on the flux reconstruction scheme to discretize unstructured hexahedral grids. The localized artificial diffusivity scheme is employed to capture shock waves robustly and to retain high-order accuracy away from the shocks. The turbulent jet flow is obtained by the FR-LAD solver using the degree of polynomial up to p=4. The computed results are in reasonable agreement with the experimental and numerical data in the literatures for time-averaged and fluctuating quantities.

Original languageEnglish
Title of host publication53rd AIAA Aerospace Sciences Meeting
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624103438
Publication statusPublished - 2015
Externally publishedYes
Event53rd AIAA Aerospace Sciences Meeting, 2015 - Kissimmee, United States
Duration: 2015 Jan 52015 Jan 9

Publication series

Name53rd AIAA Aerospace Sciences Meeting


Other53rd AIAA Aerospace Sciences Meeting, 2015
Country/TerritoryUnited States

ASJC Scopus subject areas

  • Aerospace Engineering


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