Experimental Flowfield Analyses of Installed Subsonic Jet–Pylon Interaction
Author:
Affiliation:
1. University of Southampton, Southampton, England SO17 1BJ, United Kingdom
Funder
Innovate UK
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060762
Reference19 articles.
1. Some measurements in the self-preserving jet
2. Velocity measurements in a high-Reynolds-number, momentum-conserving, axisymmetric, turbulent jet
3. Investigations of Azimuthal and Flight Effects on Noise from Realistic Turbofan Exhaust Geometries
4. WhiteD. R. “Studies into the Noise Effects Due to Pylons in Unmixed Engines,” Defence Research Agency DRA/AS/PTD/TR/94117/1, Farnborough, England, U.K. 1994.
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