LES-RANS of installed ultra-high bypass-ratio coaxial jet aeroacoustics with a finite span wing-flap geometry and flight stream - Part 2: chevron nozzle

Zhong-nan Wang; James C. Tyacke; Paul G. Tucker

doi:10.2514/6.2017-3855

LES-RANS of installed ultra-high bypass-ratio coaxial jet aeroacoustics with a finite span wing-flap geometry and flight stream - Part 2: chevron nozzle

Zhong-nan Wang, James C. Tyacke, Paul G. Tucker

Metallurgy and Materials

Research output: Contribution to conference (unpublished) › Paper › peer-review

Original language	English
DOIs	https://doi.org/10.2514/6.2017-3855
Publication status	Published - 2 Jun 2017

Access to Document

10.2514/6.2017-3855

https://arc.aiaa.org/doi/10.2514/6.2017-3855

Cite this

@conference{ec54b37c953840a6bbcfae31f7d09f03,

title = "LES-RANS of installed ultra-high bypass-ratio coaxial jet aeroacoustics with a finite span wing-flap geometry and flight stream - Part 2: chevron nozzle",

author = "Zhong-nan Wang and Tyacke, {James C.} and Tucker, {Paul G.}",

year = "2017",

month = jun,

day = "2",

doi = "10.2514/6.2017-3855",

language = "English",

}