Experimental and numerical evaluation of boundary layer ingestion effect with engine/airframe integration model

Keiichi Okai; Yoshihiro Mitani; Hidekazu Yoshida; Shotaro Ogushi; Ryosuke Tsuruta; Akiko Okuno; Tetsuya Sato; Masashi Harada

doi:10.2514/6.2019-3852

Experimental and numerical evaluation of boundary layer ingestion effect with engine/airframe integration model

Keiichi Okai, Yoshihiro Mitani, Hidekazu Yoshida, Shotaro Ogushi, Ryosuke Tsuruta, Akiko Okuno, Tetsuya Sato, Masashi Harada

School of Fundamental Science and Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

4 Citations (Scopus)

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.

Original language	English
Title of host publication	AIAA Propulsion and Energy Forum and Exposition, 2019
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)	9781624105906
DOIs	https://doi.org/10.2514/6.2019-3852
Publication status	Published - 2019
Event	AIAA Propulsion and Energy Forum and Exposition, 2019 - Indianapolis, United States Duration: 2019 Aug 19 → 2019 Aug 22

Publication series

Name	AIAA Propulsion and Energy Forum and Exposition, 2019

Conference

Conference	AIAA Propulsion and Energy Forum and Exposition, 2019
Country/Territory	United States
City	Indianapolis
Period	19/8/19 → 19/8/22

ASJC Scopus subject areas

Energy(all)
Aerospace Engineering
Electrical and Electronic Engineering
Control and Systems Engineering
Mechanical Engineering

Access to Document

10.2514/6.2019-3852

Cite this

Okai, K., Mitani, Y., Yoshida, H., Ogushi, S., Tsuruta, R., Okuno, A., Sato, T., & Harada, M. (2019). Experimental and numerical evaluation of boundary layer ingestion effect with engine/airframe integration model. In AIAA Propulsion and Energy Forum and Exposition, 2019 (AIAA Propulsion and Energy Forum and Exposition, 2019). American Institute of Aeronautics and Astronautics Inc, AIAA. https://doi.org/10.2514/6.2019-3852

Experimental and numerical evaluation of boundary layer ingestion effect with engine/airframe integration model. / Okai, Keiichi; Mitani, Yoshihiro; Yoshida, Hidekazu et al.

AIAA Propulsion and Energy Forum and Exposition, 2019. American Institute of Aeronautics and Astronautics Inc, AIAA, 2019. (AIAA Propulsion and Energy Forum and Exposition, 2019).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Okai, K, Mitani, Y, Yoshida, H, Ogushi, S, Tsuruta, R, Okuno, A, Sato, T & Harada, M 2019, Experimental and numerical evaluation of boundary layer ingestion effect with engine/airframe integration model. in AIAA Propulsion and Energy Forum and Exposition, 2019. AIAA Propulsion and Energy Forum and Exposition, 2019, American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, United States, 19/8/19. https://doi.org/10.2514/6.2019-3852

Okai K, Mitani Y, Yoshida H, Ogushi S, Tsuruta R, Okuno A et al. Experimental and numerical evaluation of boundary layer ingestion effect with engine/airframe integration model. In AIAA Propulsion and Energy Forum and Exposition, 2019. American Institute of Aeronautics and Astronautics Inc, AIAA. 2019. (AIAA Propulsion and Energy Forum and Exposition, 2019). doi: 10.2514/6.2019-3852

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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",

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doi = "10.2514/6.2019-3852",

language = "English",

isbn = "9781624105906",

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AU - Okai, Keiichi

AU - Mitani, Yoshihiro

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AU - Tsuruta, Ryosuke

AU - Okuno, Akiko

AU - Sato, Tetsuya

AU - Harada, Masashi

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N2 - 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.

AB - 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.

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Experimental and numerical evaluation of boundary layer ingestion effect with engine/airframe integration model

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