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  4. Assessment of Detached Eddy Simulation and Sliding Mesh Interface in predicting Tiltrotor Performance in Helicopter and Airplane Modes

Assessment of Detached Eddy Simulation and Sliding Mesh Interface in predicting Tiltrotor Performance in Helicopter and Airplane Modes

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sword-2022-09-20T17:59:31.original.xml (130 B)
Original SWORD entry document
Author(s)
Jia, Feilin
•
Moore, John
•
Wang, Qiqi
Date Issued
2021
Journal
AIAA AVIATION 2021 FORUM
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Citation
Jia, Feilin, Moore, John and Wang, Qiqi. 2021. "Assessment of Detached Eddy Simulation and Sliding Mesh Interface in predicting Tiltrotor Performance in Helicopter and Airplane Modes." AIAA AVIATION 2021 FORUM.
Version
Author's final manuscript
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
Creative Commons Attribution-Noncommercial-Share Alike
http://creativecommons.org/licenses/by-nc-sa/4.0/
Persistent DSpace Link
https://hdl.handle.net/1721.1/145535
DOI of Published Version
https://doi.org/10.2514/6.2021-2601
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