@inproceedings{75c6ec4a3acd4a87886c703c6bf33daa,
title = "Experimental and numerical evaluation of boundary layer ingestion effect with engine/airframe integration model",
abstract = "Boundary layer ingestion benefit is experimentally and numerically investigated. Simple 2-dimensional-airfoil shape airframe with electric fan configures an airframe/engine integration. Wind tunnel test was conducted with force measurement. Accompanying CFD calculation was conducted with a solver FaSTAR developed by JAXA. Experimental result shows that both of the 2 BLI configurations give larger forward thrust than referential nonBLI configuration with same power consumption. The difference between the 2 BLI case results was investigated. CFD result shows quantitative agreement with the experimental result, though performance metrics is different.",
author = "Keiichi Okai and Yoshihiro Mitani and Hidekazu Yoshida and Shotaro Ogushi and Ryosuke Tsuruta and Akiko Okuno and Tetsuya Sato and Masashi Harada",
note = "Publisher Copyright: {\textcopyright} 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA Propulsion and Energy Forum and Exposition, 2019 ; Conference date: 19-08-2019 Through 22-08-2019",
year = "2019",
doi = "10.2514/6.2019-3852",
language = "English",
isbn = "9781624105906",
series = "AIAA Propulsion and Energy Forum and Exposition, 2019",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA Propulsion and Energy Forum and Exposition, 2019",
}