Numerical Investigation of Installed Jet Noise Sensitivity to Lift and Wing/Engine Positioning
Author:
Affiliation:
1. Loughborough University
Publisher
American Institute of Aeronautics and Astronautics
Reference27 articles.
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3. Tyacke, J. C., Wang, Z.N., and Tucker, P. G. “LES-RANS of installed ultra-high bypass-ratio coaxial jet aeroacoustics with a finitespanwing-flapgeometryandflightstream-Part1: roundnozzle,”2017. doi:10.2514/6.2017-3854.
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